43 Msc Nastran Jobs

Job Description Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Provide execution insight and facilitate the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Understand the meshing and analysis guidelines for static and fatigue analysis and ensure the FE models created by team for F&DT justifications are compiled to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the specific considerations for the fatigue evaluation is correctly captured and simulated in the FE models and if required use your expertise and guidance to align with the requirements. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Identify the fatigue critical locations based on highly stressed areas from static analysis results, safety critical parts and the standard features which irrespective of stress value need to be checked. Down select the number of calculation points and align with the client on this. Decision basis for selection of reliable concepts out of multiple concepts based on the static and F&DT justification validations and compliance including future operational and maintenance and repair considerations. Enable F&DT team with expertise for generation of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Review the outputs. Level II checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Technically lead and guide the team for mitigating the low fatigue and crack growth life and F&DT performance non-compliance issues based on your expertise and experience. Align these methods with clients and document it as reference documents. Incorporate features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Technically lead for aligning customer expectations with engineering deliverables and strategic goals. Collaborate and lead cross-functionally with design manufacturing quality, and systems teams. Technical interface with the client, ensuring timely issue resolutions, aligning design mitigations and any deviations needed w.r.t processes, methods, inputs, and deliverables. Professional & Technical Skills:Expertise and work experience in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from F&DT point of view. Experience of implementing the weight optimization techniques, load path optimization, fatigue and damage tolerance analysis for helicopter/aircraft certification and testing activities. Knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of F&DT test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing aircrafts. Exposure to certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Any experience in process automation using MS excel VBA/Python etc Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistrucut. or similar tools is a strong plus. Automation experience using Excel MACROS & VBA Python and CATIA V5 is a plus. Proven experience for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Working experience related to aircraft materials, fatigue phenomenon, fracture mechanics concepts, fatigue spectrum derivation, probabilistic fatigue and crack growth assessments. Sound knowledge of primary and secondary load paths, structural classification and their relevance for the F&DT justification. Expertise in structural classification, related F&DT compliance, calculation points and their down selection, selection of scatter factors. Deep knowledge of FEA considerations and their incorporation in the meshing requirements for F&DT Analysis. Experience in end-to-end concept to design validation, manufacturability, certification and F&DT certification test and test correlation activities for preferably rotary wing aircraft helicopter certification. In-depth understanding of helicopter/aircraft load-bearing structures, structural response with focus on structural integrity, stiffness, and load path optimization under both static and Fatigue conditions. Knowledge of failure modes relevant to metallic and composite airframe components. Experience for low cycles and high cycle fatigue analysis for fixed wing or rotary wing aircrafts. Exposure to functional considerations like telescopic, foldability swivel and reversal of structure. Any specialization/certification in F&DT/Fracture mechanics/fatigue life extension etc will be a plus. Additional Information:- The candidate should have 9 to 12 years of practical experience in the Aerostructures fatigue and damage tolerance analysis domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Job Description Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NA Minimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Independently execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Perform the static FEA independently for fatigue loading to facilitate the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Follow the meshing and analysis guidelines for static and fatigue analysis and ensure the FE models created by team for F&DT justifications are compiled to the guidelines and are of high quality. Perform the FEA V&V checks and prepare the V&V documents capture the required checks for the FE models. Also ensure the specific considerations for the fatigue evaluation is correctly captured and simulated in the FE models and if required use your expertise and guidance to align with the requirements. Independently develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Prepare detailed output which will help to Identify the fatigue critical locations based on highly stressed areas from static analysis results, safety critical parts and the standard features which irrespective of stress value need to be checked. Perform the low RF/MOS mitigation, Alternative concepts analyses, compilation of inputs for the review and certification reports. Down select the number of calculation points and align with the client on this in alignment with SME/Team leads. Perform the required analyses checks to enable decision basis for selection of reliable concepts out of multiple concepts based on the static and F&DT justification validations compliance including future operational and maintenance and repair considerations. Enable F&DT team with required inputs for generation of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Review the outputs. Peer checker for F&DT analysis certification task. Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Perform the mitigation task for the low fatigue, crack growth life and F&DT performance non-compliance issues based on your expertise and experience. Align these methods with SMEs team leaders and document it as reference documents. Perform tasks as required based on the outcomes of Collaboration with cross-functional discussions with design manufacturing quality, and systems teams; actively support with relevant detailed results and observations to engage in design reviews, issue resolution, and integration discussions. Assisting customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Enable aligning customer expectations with engineering deliverables and strategic goals. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from F&DT point of view. Experience of static and F&DT analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization, fatigue and damage tolerance analysis for helicopter/aircraft certification and testing activities. Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of F&DT test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistrucut. or similar tools is a strong plus. Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. Expertise for structural sizing of aerospace structural parts meeting certification, testing and manufacturability requirements. Sound work experience related to aircraft materials, fatigue phenomenon, fracture mechanics concepts, fatigue spectrum derivation, probabilistic fatigue and crack growth assessments. Must have knowledge of structural classification, primary and secondary structure design requirements, load path and structural response. Perform the low RF/MOS mitigation, Alternative concepts analyses, compilation of inputs for the review and certification reports. Expertise in structural classification, related F&DT compliance, calculation points and their down selection, selection of scatter factors. FEA considerations and their incorporation in the meshing requirements for F&DT Analysis. In-depth understanding of helicopter/aircraft load-bearing structures, structural response with focus on structural integrity, stiffness, and load path optimization under both static and Fatigue conditions. Knowledge of failure modes relevant to metallic and composite airframe components. Proven experience for low cycles and high cycle fatigue analysis for fixed wing or rotary wing aircrafts. Exposure to functional considerations like telescopic, foldability swivel and reversal of structure. Additional Information:- The candidate should have 5 to 8 years of practical experience in the Aerostructures fatigue and damage tolerance analysis domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Provide execution insight and facilitate the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Understand the meshing and analysis guidelines for static and fatigue analysis and ensure the FE models created by team for F&DT justifications are compiled to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the specific considerations for the fatigue evaluation is correctly captured and simulated in the FE models and if required use your expertise and guidance to align with the requirements. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Identify the fatigue critical locations based on highly stressed areas from static analysis results, safety critical parts and the standard features which irrespective of stress value need to be checked. Down select the number of calculation points and align with the client on this. Decision basis for selection of reliable concepts out of multiple concepts based on the static and F&DT justification validations and compliance including future operational and maintenance and repair considerations. Enable F&DT team with expertise for generation of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Review the outputs. Level II checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Technically lead and guide the team for mitigating the low fatigue and crack growth life and F&DT performance non-compliance issues based on your expertise and experience. Align these methods with clients and document it as reference documents. Incorporate features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Technically lead for aligning customer expectations with engineering deliverables and strategic goals. Collaborate and lead cross-functionally with design manufacturing quality, and systems teams. Technical interface with the client, ensuring timely issue resolutions, aligning design mitigations and any deviations needed w.r.t processes, methods, inputs, and deliverables. Professional & Technical Skills:Expertise and work experience in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from F&DT point of view. Experience of implementing the weight optimization techniques, load path optimization, fatigue and damage tolerance analysis for helicopter/aircraft certification and testing activities. Knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of F&DT test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing aircrafts. Exposure to certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Any experience in process automation using MS excel VBA/Python etc Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistrucut. or similar tools is a strong plus. Automation experience using Excel MACROS & VBA Python and CATIA V5 is a plus. Proven experience for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Working experience related to aircraft materials, fatigue phenomenon, fracture mechanics concepts, fatigue spectrum derivation, probabilistic fatigue and crack growth assessments. Sound knowledge of primary and secondary load paths, structural classification and their relevance for the F&DT justification. Expertise in structural classification, related F&DT compliance, calculation points and their down selection, selection of scatter factors. Deep knowledge of FEA considerations and their incorporation in the meshing requirements for F&DT Analysis. Experience in end-to-end concept to design validation, manufacturability, certification and F&DT certification test and test correlation activities for preferably rotary wing aircraft helicopter certification. In-depth understanding of helicopter/aircraft load-bearing structures, structural response with focus on structural integrity, stiffness, and load path optimization under both static and Fatigue conditions. Knowledge of failure modes relevant to metallic and composite airframe components. Experience for low cycles and high cycle fatigue analysis for fixed wing or rotary wing aircrafts. Exposure to functional considerations like telescopic, foldability swivel and reversal of structure. Any specialization/certification in F&DT/Fracture mechanics/fatigue life extension etc will be a plus. Additional Information:- The candidate should have 9 to 12 years of practical experience in the Aerostructures fatigue and damage tolerance analysis domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Minimum 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Lead and oversee the execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Guide the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Establish and govern engineering F&DT analysis best practices, design review frameworks, and technical quality gates across the program lifecycle. Provide technical oversight related to F&DT across multiple concept development, structural architecture, F&DT requirement compliance for detailed design, integration, certification and certification test support. Support in generation and review of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Level II and level III checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Lead root cause investigations, risk assessments, and resolution strategies for stress/F&DT related issues, non-conformances, schedule variance and airworthiness deviations. Finalize the F&DT technical requirements, limitations and associated tasks within defined timelines, ensuring high-quality output with minimal errors. Analyse complex design challenges and propose optimal engineering solutions aligned with project goals and constraints. Provide high level competency for the fatigue spectrum derivation for analysis and the subsequent service load and the test load spectrum derivation. Document the procedure as a signed document for reference. Supervision and approval of method register, F&DT method document, Analysis tools alignment, F&DT certification analysis check lists, certification test report templates and SLA in alignment with client during the initial execution phase. Act as the technical voice of the program, aligning customer expectations with engineering deliverables and strategic goals. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Lead effective engineering change management by proactively tracking evolving inputs and shifting requirements. Evaluate and mitigate the impact of delays on schedule variance, resource planning, costs, and milestone achievement through a structured change control process aligned with client approvals and established governance protocols. Represent engineering during customer technical audits, program quality gate reviews, and change control reviews. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Act as the primary technical/program level interface with the client, ensuring alignment on F&DT compliance objectives and deliverables. Professional & Technical Skills:Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have minimum 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 7.5 Year(s) Of Experience Is Required Educational Qualification : 15 years full time education Summary: As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities: Join a mid-level leadership role within the Aerostructure Engineering team, supporting both strategy and technical execution across the full engineering lifecyclefrom concept through production, certification, and sustainment. Play a pivotal role in leading engineering delivery, technical governance, and client interactions for high-impact aerospace programs spanning rotary- and fixed-wing platforms. Opportunity to drive digital engineering initiatives including MBD, MBSE, and digital twin integration within legacy and next-gen design environments. Own design and development tasks for aircraft structural components. Apply advanced aircraft structural analyses Approach to Validate the design concepts through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection and operational / design / environmental conditions compliant to the airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Preparation of method register, Method document, check lists, report templates, SLA in alignment with client. Guide the team for selection of optimum design by stress evaluation of multiple structural design concepts through detailed trade-off analyses for required dimensions and weight constraints. Maintaining scope / requirement log, Input / enabler and query trackers and coordinating with respective client stakeholders to get the resolutions on-time, ensuring high-quality output. Lead the team to develop complex 2D and 3D FE models, their integration, properties allocation, create validation and verification reports for the FE models, Analysis deck preparation/editing, perform structural Analyses, result extraction and interpretations, Error removal, post process and assist in developing automation using inhouse macros. Finalize the meshing and analyses requirements for different types of structural analyses in alignment with client. Mitigation in case of low RF/MOS, Alternative concepts analyses, compilation of inputs for the review and certification reports. Analyse complex design challenges and propose optimal engineering solutions. Level II and Level III checker and signatory for the analysis and certification reports from Accenture side. Certification test support creation of FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Ensuring alignment with weight budgets and performance criteria. Collaborate and lead cross-functionally with design team, manufacturing, quality, and systems teams; actively engage in design reviews, issue resolution, and integration discussions. Act as the primary technical interface with the client, ensuring alignment on design objectives and deliverables. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills: Expertise in the design, development and integration of metallic, and composite helicopter / aircraft structures for both primary and secondary components from static / Dynamic/ Impact point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Working knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Familiarity with GD&T and industry drawing standards, Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ Optistruct /LS DYANA is must, Can guide the team for automation using Excel MACROS & VBA / Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analysis. End to end concept to design validation, certification, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft / helicopter. Command over the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Strong grasp of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. In-depth understanding of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. Deep knowledge of rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information: - The candidate should have a 12 to 15 years of experience in the Aerostructure Analysis domain preferably for the rotary wing aircrafts, in a technical managerial & program manager role for OEM/service providers. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day. - A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Show more Show less

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 5 Year(s) Of Experience Is Required Educational Qualification : 15 years full time education Summary: As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities: You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29 /CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational / design / environmental conditions. Owning optimum design by static stress analysis / Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF / Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills: Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter / aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel / VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ Optistruct /LS DYANA is must, Automation experience using Excel MACROS & VBA / Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft / helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information: - The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day. - A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Show more Show less

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 3 Year(s) Of Experience Is Required Educational Qualification : 15 years full time education Summary: As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities: You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Use meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform FEA analysis for static dynamic and impact analysis in alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29 /CS/JAR/Military MIL-STD-1530 etc Take up team engagements and knowledge sharing sessions for distributed teams across the programs and locations. Design validation of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational / design / environmental conditions. Document the details for presenting into the certification reports and certifying agencies. Provide supporting evidence for the selection of optimum design by static stress analysis / Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Comply to schedule, weight requirement and cost compliance by efficiently tracking methods. Follow escalation mechanism to ensure compliance. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Provide analysis results for the decision process of selection of reliable concepts out of multiple concepts based on the static, dynamic and impact stress analysis validation with future operational and maintenance and repair considerations. Provide details from FE models for the weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Perform the task of mitigating the low RF / Low life and performance non-compliance issues based on discussion with SME/Leads or your expertise and experience. Align relevant details of these methods to SME/Leads to align with the client. Documentation of iterations and outcomes for future reference. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Design validate through analysis or classical calculations the Incorporated features and design aspects covering the downstream manufacturing and inspection processes, accessibility and in-service replacement/repair. Prepare detailed presentation for reference and review. Assist in during customer technical audits, program quality gate reviews, and change control reviews by providing the required analysis results and justifications. Professional & Technical Skills: Experience with Aerospace projects for the design/development and integration of metallic, and composite helicopter / aircraft structures for both primary and secondary components. Knowledge of Aerospace structures, their classification as primary, secondary and support structures based on load bearing capacities. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Exposure to weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Experience in process automation using MS excel / VBA/Python etc Exposure to airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Knowledge of Preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Knowledge of certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ Optistruct /LS DYANA is must, Automation experience using Excel MACROS & VBA / Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. FEA V&V methods, analysis as per the certification compliance, manufacturing support and certification. Create inputs for the test & test correlation activities specifically for rotary wing aircraft / helicopter. Experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material, structural feature simulation, analyses as per meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis, analysis error and post processing of Analysis results. knowledge of helicopter/aircraft load-bearing structures Experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Familiarity with Fatigue requirement is plus. Experience in static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Exposure to Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Knowledge of structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Additional Information: - The candidate should have a 5 to 8 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day. - A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Show more Show less

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary : As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities: You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills: Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NA Minimum 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Lead and oversee the execution of comprehensive fatigue and damage tolerance analysis for metallic and composite structural parts related to design and development of rotary wing aircrafts primary and secondary structures. Guide the team with interpretation of static analysis results for defining the fatigue critical location, number of calculation points, fatigue sensitive area, primary and secondary load path identification, design philosophy identification, scatter factor selection in alignment with client and regulatory guidelines FAR/CS 25.571, 29.571, MIL-STD-1530 etc. Establish and govern engineering F&DT analysis best practices, design review frameworks, and technical quality gates across the program lifecycle. Provide technical oversight related to F&DT across multiple concept development, structural architecture, F&DT requirement compliance for detailed design, integration, certification and certification test support. Support in generation and review of fatigue test plan (full scale and component level test), interpretation of test results and correlation with analysis in the test report. Level II and level III checker approver signatory for F&DT analysis certification reports, F&DT test plan, test orders and F&DT test reports. Lead root cause investigations, risk assessments, and resolution strategies for stress/F&DT related issues, non-conformances, schedule variance and airworthiness deviations. Finalize the F&DT technical requirements, limitations and associated tasks within defined timelines, ensuring high-quality output with minimal errors. Analyse complex design challenges and propose optimal engineering solutions aligned with project goals and constraints. Provide high level competency for the fatigue spectrum derivation for analysis and the subsequent service load and the test load spectrum derivation. Document the procedure as a signed document for reference. Supervision and approval of method register, F&DT method document, Analysis tools alignment, F&DT certification analysis check lists, certification test report templates and SLA in alignment with client during the initial execution phase. Act as the technical voice of the program, aligning customer expectations with engineering deliverables and strategic goals. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Lead effective engineering change management by proactively tracking evolving inputs and shifting requirements. Evaluate and mitigate the impact of delays on schedule variance, resource planning, costs, and milestone achievement through a structured change control process aligned with client approvals and established governance protocols. Represent engineering during customer technical audits, program quality gate reviews, and change control reviews. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Act as the primary technical/program level interface with the client, ensuring alignment on F&DT compliance objectives and deliverables. Professional & Technical Skills:Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO FRANC 3D MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have minimum 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

Job Description Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29CS/JAR/Military MIL-STD-1530 etc Enable team engagements and knowledge sharing for distributed teams across the programs and locations. Validate the design of structural through Classical and FE Analysis, and assist in detailed load path analysis, optimal material selection based on Analysis results and operational design environmental conditions. Owning optimum design by static stress analysis Dynamic analysis and impact analysis evaluation of multiple structural design concepts through detailed trade-off analyses. Develop 3D and 2D FE models using specified software, adhering to industry and customer-specific modelling and analysis standards and guidelines. Perform weight estimation, its tracking, and control across all design phases, ensuring alignment with weight budgets and performance criteria. Technically lead and guide the team for mitigating the low RF Low life and performance non-compliance issues. Create the test FE models incorporating the failure, features and boundary conditions as per standard procedure and test fixture. Creating the method register, Method document, check lists and report templates in compliance with regulatory and client specific requirements. Front end and act as the technical interface with the client, ensuring alignment on deviations and processes, methods, inputs, overall objectives and deliverables. Interact with clients on a regular basis to track and classify the issues and ensure timely resolution of the issues as per SLA. Assist in during customer technical audits, program quality gate reviews, and change control reviews. Support and mentor junior team members by providing technical guidance, sharing best practices, and fostering their growth in design methodologies, tools, and domain knowledge. Actively contributes to skill development, knowledge transfer, and team capability building through hands-on support and constructive feedback. Professional & Technical Skills:Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter aircraft structures for both primary and secondary components from Static point of view. Experience of static dynamic and impact analysis for sizing of large, fixed wing or rotary wing aircraft. Experience in weight optimization techniques, load path optimization for helicopter/aircraft certification and testing activities. Any experience in process automation using MS excel VBA/Python etc Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of full scale and component level certification test plan, test orders, test load derivation and test to analysis correlation reports for component level for fixed wing or rotary wing aircrafts. Certification testing and test correlation, life extension and fatigue resistant structure design. Familiarity with GD & T and drawing standards. Proficiency over the structural static dynamic and impact analysis tools like general MSC NASTRAN/PATRAN/ABAQUS/ HyperMesh/ OptistructLS DYANA is must, Automation experience using Excel MACROS & VBA Python and Catia V5 is a plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analyses. End to end validation, certification compliance, manufacturing support and certification test & test correlation activities specifically for rotary wing aircraft helicopter. High level skills and experience in the 2D/3D mesh creation and meshing guidelines, FE Modelling, and Assembly integration methodologies. Experience of aerospace material selection, structural feature simulation, analyses and meshing guidelines and procedures. Capability to solve day to day analysis problem in Analysis and post processing of Analysis results. Sound knowledge of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Familiarity with Fatigue requirement is plus. High experience aligned with the rotary wing or fixed wing structural arrangement, primary, secondary and support structures, load path, sizing procedures for metallic and composite structures. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Introductory knowledge about the analysis considerations for the any of the Innovative design and functional considerations like telescopic structures, foldability swivel and reversal of structure. Expertise for structural sizing of aerospace and rotary wing aircraft structural parts meeting certification, testing and manufacturability requirements. Familiar with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Additional Information:- The candidate should have a 8 to 9 years of practical experience static analysis/Dynamic analysis/ Impact Analysis in the Aerostructures domain, preferably with exposure to rotary-wing aircraft platforms and full design cycle involvement. - This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

About The Role Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NAMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Support in the design validation through static dynamic and impact analysis of rotary wing aircraft structural components. Work under the guidance of the Lead Engineer to develop complex 2D and 3D FE models, their integration, properties allocation, validation and verification of FE models, Analysis deck preparation/editing, perform different structural Analyses, result extraction and post processing using inhouse macros. Use meshing and analysis guidelines for static, dynamic and impact analysis FE model creation and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform the required analyses task under supervision for the low RF/MOS mitigation, Alternative concepts analyses, creation of inputs for the review and certification reports. Address design challenges and implement the proposed optimal engineering solutions aligned with project goals and constraints. Apply basic principles of aerospace structures design /sizing and material selection. Interpret technical requirements and execute assigned tasks within defined timelines, ensuring high-quality output with minimal errors. Assist in interpreting technical requirements and validate it through justification analyses. Participate in design reviews and incorporate feedback into iterative improvements. Collaborate with cross-functional teams to ensure alignment with structural and performance goals. Engage in training sessions to enhance technical knowledge and skillsets relevant to the role. Professional & Technical Skills: Good experience of 2D/3D mesh creation and meshing guidelines, FE Modeling, and Assembly integration methodologies. Experience of static dynamic and impact analysis for sizing of large, fixed-wing or rotary wing aircraft for major OEMs. Knowledge of classical hand calculations for simple structural parts Command over MSC NASTRAN/PATRAN/ Hypermesh/ Optistruct is must F&DT knowledge, Excel MACROS using VBA / Python and Catia V5 is a plus Understanding of Engineering Drawings and Analysis data extraction from CAD models. Must have knowledge of structural classification, primary and secondary structure design requirements, load path and structural response Additional Information:- The candidate should have a 2 to 4 years of experience in the Aerostructure Analysis domain. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

About The Role Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Support in the design validation through static dynamic and impact analysis of rotary wing aircraft structural components. Work under the guidance of the Lead Engineer to develop complex 2D and 3D FE models to be used for the fatigue evaluations, their integration, properties allocation, validation and verification of FE models, Analysis deck preparation/editing, perform different structural Analyses, result extraction and post processing using inhouse macros. Use meshing and analysis guidelines for fatigue and DT analysis FE model creation and ensure the FE models created by team are compiled to the guidelines and are of high quality. Perform the checks and prepare FEA V&V documents, capture the required checks for the FE models. Also ensure the physics of the problem as applicable for the fatigue life and crack growth estimations is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Perform the required analyses task under supervision for the low LIFE/RF/MOS mitigation, Alternative concepts analyses, creation of inputs for the review and certification reports. Use Excel macros and program codes to extract and post process the required data from FEA output files for further F&DT evaluation. Address design challenges and implement the proposed optimal engineering solutions aligned with project goals and constraints. Apply basic principles of aerospace structures design /sizing and material selection to meet the project goals. Familiarize with the structural classification, primary and secondary structure design requirements, load path and structural response. Interpret technical requirements and execute assigned tasks within defined timelines, ensuring high-quality output with minimal errors. Assist in interpreting technical requirements and validate it through justification analyses. Participate in design reviews and incorporate feedback into iterative improvements. Participate in the cross-functional teams to ensure alignment with structural and performance goals. Engage in training sessions to enhance technical knowledge and skillsets relevant to the role. Professional & Technical Skills: Technical Skills: Strong command over the 2D/3D mesh creation and meshing guidelines, FE Modeling, and Assembly integration methodologies. Command over MSC NASTRAN/PATRAN/ HyperMesh/ Optistruct is must and F&DT knowledge, Excel MACROS using VBA / Python and Catia V5 is a plus Understanding of Engineering Drawings and Analysis data extraction from CAD models. Professional Attributes:Self-motivated, quick to learn, well-organized, and capable of independently planning and executing tasks with minimal supervision. Additional Information:- The candidate should have 2 to 4 years of experience in the Aerostructure Analysis domain. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

About The Role Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 7.5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Join a mid-level leadership role within the Aerostructure Engineering team, supporting both strategy and technical execution across the full engineering lifecyclefrom concept through production, certification, and sustainment. Play a pivotal role in leading engineering delivery, technical governance, and client interactions for high-impact aerospace programs spanning rotary- and fixed-wing platforms. Opportunity to drive digital engineering initiatives including MBD, MBSE, and digital twin integration within legacy and next-gen design environments. Lead fatigue and damage tolerance (F&DT) analysis for metallic/composite parts in primary and secondary rotary wing structures. Guide interpretation of static analysis to define fatigue-critical areas, calc points, load paths, design intent, and scatter factors per FAR/CS 25.571/29.571, MIL-STD-1530, etc. Prepare method registers, F&DT documents, tool alignment, certification checklists, test report templates, and SLAs per scope and client needs. Manage project scope, constraints, and alignments with client during project initiation. Apply standard F&DT methods and best practices, documenting limitations based on NDE/NDI, manufacturing constraints, and design criteria. Provide expertise in deriving fatigue and test load spectra and formalize via documented procedures. Offer technical oversight across concept design, structural layout, compliance checks, integration, certification, and test phases. Support fatigue test plan creation (full/component level), test result interpretation, and correlation; review team outputs. Act as Level II/III checker, approver, and signatory for F&DT analysis, plans, test orders, and reports. Lead root cause investigations, risk assessments, and resolution of stress/F&DT issues, non-conformances, and airworthiness gaps. Analyze complex design issues and recommend optimal engineering solutions aligned with program goals. Support delivery manager and act as the technical voice of the program, enable aligning customer expectations with engineering deliverables and strategic goals. Front face Accenture in all technical discussions and lead the discussion. Drive end-to-end scope definition, requirements management, and traceability across the engineering structural lifecycle related to F&DT justification. Ensure effective planning, milestone tracking, and schedule variance analysis to maintain alignment with program delivery goals and importantly internal deal construct parameters or solution baselines. Drive robust engineering change management by closely monitoring evolving inputs and requirement changes. Assess and manage the impact of delays on schedule variance, resource allocation, cost, and milestone delivery through a structured change control process aligned with client approvals and governance protocols. Ensure engineering activities meet cost, schedule, target weight and performance objectives while maintaining traceability and regulatory compliance. Collaborate and lead cross-functionally with design/analysis team, manufacturing, quality, and systems teams; actively engage in design reviews, issue resolution, and integration discussions. Act as the technical interface with the client, ensuring alignment of F&DT compliance objectives and deliverables. Professional & Technical Skills: Expertise in design, development, and integration of metallic and composite helicopter/aircraft structures (primary and secondary) from F&DT perspective. Experience with static and F&DT analysis for sizing large fixed or rotary wing aircraft. Skilled in weight and load path optimization, fatigue, and damage tolerance for certification and testing. Strong knowledge of airworthiness regulations (CS-27/29, FAR 23/25), OEM standards, and FAA/EASA certification. Experienced in test plan preparation, test orders, load derivation, and test-to-analysis correlation for component and full-scale tests. Familiar with certification testing, life extension, and fatigue-resistant structure design. Knowledge of GD&T and drawing standards is a plus. Proficient in FEA and F&DT tools is essential with experience in NASGRO / FRANC 3D / MSC FATIGUE, MSC NASTRAN/PATRAN, HyperMesh/Optistruct. or similar tools is a strong plus. Can guide the team for automation using Excel MACROS & VBA / Python and Catia V5 is a plusDeep understanding of aircraft materials, fatigue, fracture mechanics, fatigue spectrum derivation, and probabilistic crack growth assessment. Familiar with FEA considerations and meshing for F&DT analysis. Experience from concept through design validation, manufacturability, certification, and F&DT test correlation, preferably for rotary wing aircraft. Strong knowledge of helicopter/aircraft load-bearing structures, focusing on integrity, stiffness, and load path optimization under static and fatigue loads. Awareness of failure modes in metallic and composite airframe parts. Skilled in structural classification, F&DT compliance, calculation points, down-selection, and scatter factor selection. Proven expertise in low and high cycle fatigue analysis for fixed or rotary wing aircraft. Acoustics and noise separation knowledge is a plus. Competent in structural sizing to meet certification, test, and manufacturability requirements. Proven experience in static and F&DT sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems and qualitywithin complex delivery frameworks for aerostructure development programs. Additional Information:- The candidate should have 12 to 15 years of engineering experience in the Aerostructures F&DT domain preferably for the rotary wing aircrafts, technical managerial & program manager role for OEM/service providers. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

About The Role Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NAMinimum 12 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities:Lead strategic aerospace engineering engagements for rotary wing platforms, driving technical delivery, innovation, and client satisfaction. Play a key role in shaping engineering processes, delivery governance, and team capability development. Engage directly with aerospace OEMs, Tier-1 suppliers and regulatory bodies, influencing design decisions, compliance strategies, and product lifecycle outcomes. Drive digital engineering transformation, championing initiatives around MBSE, MBD, and digital continuity. Oversee static, dynamic, and impact sizing analysis for primary/secondary rotary wing structures. Establish engineering best practices, review frameworks, and quality gates. Provide oversight across concept development, stress validation, integration, and certification. Plan analysis/test requirements for metallic and composite materials, ensuring structural integrity and compliance. Act as Level II/III checker or approver for analysis reports and test documentation. Integrate cost, weight, safety, and manufacturability into design lifecycles. Lead root cause investigations, risk assessments, and corrective actions for structural issues. Finalize technical requirements within timelines and ensure high-quality outputs. Developing L3 level planning compliant to program milestones and driving scope / requirements and Input management accordingly to meet defined planning. Establish method documents, report templates, and SLAs during project setup. Drive scope definition, requirement traceability, and analysis across the structural lifecycle. Represent Accenture in technical discussions, aligning deliverables with client expectations. Lead discussions on analysis methods, meshing, and sizing guidelines. Track milestones, manage schedules, and ensure alignment with program goals. Monitor evolving requirements, manage changes, and ensure compliance with cost/schedule targets. Act as the key technical liaison, ensuring clarity and alignment on project deliverables. Build and mentor a high-performance engineering team with clear vision and growth plans. Conduct coaching, reviews, and succession planning. Contribute to internal initiatives, including design automation and digital workflows. Proven experience in static dynamic and impact analysis / sizing for design and integration of rotary-wing and/or fixed-wing aircraft structures across end-to-end design lifecycle phases. Demonstrated experience collaborating with cross-functional teamsincluding design, stress analysis, manufacturing, systems integration and quality within complex delivery frameworks for aerostructure development programs. Bachelors / masters degree (BE/MTech) in Aerospace, Aeronautical, or Mechanical Engineering. Certifications in project management (PMP/Prince2), Six Sigma, or Digital Engineering will be plus. FEA considerations and meshing requirements for different types of structural analyses like static, dynamic, buckling and impact analysis. In-depth understanding of helicopter/aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static, dynamic, and impact conditions. Strong awareness of static dynamic and impact strength justification analyses and failure modes relevant to metallic and composite airframe components. Familiarity with structural analysis considerations related to assembly line constraints, ergonomic considerations, and sequence planning to ensure seamless integration in high-rate production environments. Proficient in configuration management principles, including part lifecycle management, engineering change control, version tracking, and release processes will be plus. Professional & Technical Skills: Expertise in the design/development and integration of metallic, sheet metal, and composite helicopter / aircraft structures for both primary and secondary components. Experience in weight optimization techniques, load path optimization, helicopter/aircraft certification and testing activities. Strong knowledge of airworthiness compliance regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Experience in preparation of test plan, test orders, test load derivation and test to analysis correlation reports for component level and full-scale structural tests for rotary wing / fixed wing aircrafts. Experience managing design-to-cost, design-to-weight, and sustainability considerations across the design lifecycleProficient in common FEA tools is essential with experience in MSC NASTRAN/PATRAN, ABAQUS, HyperMesh/Optistruct. LS DYANA or similar tools is a strong plus. Technically sound, solution-driven leader with strong decision-making skills. Capable of guiding teams through complexity and ambiguity. Strong communicator and client interface, capable of aligning stakeholders. Passionate about mentoring and driving engineering excellence. Strategic mindset focused on quality, optimization, and best practices. Additional Information:- The candidate should have a minimum of 15 years of engineering experience in the Aerostructures domain, with at least 5 years in a technical leadership or program governance role. This position is based at client location Bengaluru and 6 days a workweek requiring 8 working hours per day.- A B Tech/M Tech in Aerospace, Aeronautical, or Mechanical Engineering is required Qualification 15 years full time education

As a Specialist Simulation Engineer focusing on Durability at Volvo Group, you will be responsible for leading advanced simulation activities to provide engineering insights that support robust design decisions and contribute to digital transformation within product development. Your key responsibilities will include ensuring simulation accuracy and reliability by applying best practices, developing durable design solutions meeting performance targets, conducting structural simulations, performing fatigue life predictions, leading design optimization studies, proposing new simulation methodologies, correlating simulation results with physical test data, and collaborating across global teams throughout the product development lifecycle. Additionally, you will leverage data analytics to refine simulation fidelity and influence key design decisions in the durability domain. To excel in this role, you must possess a Master's degree in Mechanical Engineering, Automotive Engineering, or a related field, along with a minimum of 12 years of CAE experience in the automotive industry focusing on product development and durability. You should have proven experience leading durability simulation programs across multiple vehicle platforms, in-depth understanding of fatigue mechanics, proficiency in tools such as MSC Nastran, ABAQUS, HyperWorks, nCode (or equivalent), and Beta-CAE, and experience with optimization techniques for mass and cost efficiency in engineering designs. Furthermore, you should have familiarity with physical testing, test-simulation correlation, and validation processes, be innovation-driven with a history of filed patents and implementation of industrialized solutions, and possess strong collaboration skills, attention to detail, and a proactive approach to continuous improvement. Soft skills such as a strong sense of ownership, excellent communication, fast learning ability, team-oriented mindset, and methodical problem-solving approach will be essential for success in this role. If you are passionate about shaping sustainable transportation solutions for the future, working with cutting-edge technologies, and being part of a collaborative team that leaves a positive impact on society, then this position at Volvo Group could be the perfect match for you.,

Transport is at the core of modern society. Imagine using your expertise to shape sustainable transport and infrastructure solutions for the futureIf you seek to make a difference on a global scale, working with next-gen technologies and the sharpest collaborative teams, then we could be a perfect match. What you will do At (ENTITY) you will contribute to the transformation of our company, the transport industry and society at large. You will: List here the main mission and responsibilities. Describe the context of the role in one sentence. Give the candidates a broad understanding of what they would do and deliver. No need to be exhaustive, focus on what s new, different, or exciting about this role and describe it with strong action verbs (e. g. leading, overseeing, developing, creating). Give a taste of the projects they ll be working on and who they ll collaborate with. Your future team Describe your team in a sentence or two: number of members, roles, backgrounds, team culture in other words, your team selling points. As an option, you can include here a photo or a video of your team welcoming candidates or describing what they like best working here. You can do that with your own phone, as a team building exercise. It will guarantee you great attention! Who are you Do you dream bigWe do too, and we are excited to grow together. In this role, you will bring: List here the job requirements in terms of skills, knowledge, and experience but also mindset and motivation. Separate between essential requirements (4 to 6 maximum) which would disqualify any candidate, and nice to have characteristics. Ask yourself if your expectations are inclusive of all possible candidates in terms of gender, nationality, personality etc. What s in it for you We offer a solid package of compensation and benefits, plus you will enjoy: This bullet-pointed section should answer the following questions. You may ask team members what they enjoy. Describe how you care for people and value their wellbeing. Talk about the atmosphere in the team together with the flexible arrangements and work life balance you offer. Highlight the opportunities to develop, build a career and work globally or cross-functionally. Relate to location, physical work environment and services on site when they are selling points. Ready for the next move Select one of these calls to action or mix them or phrase your personal invitation: If you are curious to explore how we put our words into actions, follow us on LinkedIn and volvogroup. com. If you want to make a real impact in your career, the transportation business is where you want to be. We look forward to meeting you. Are you excited to bring your skills and disruptive ideas to the tableWe can t wait to hear from you. Apply today! Come join us for a cup of coffee or a call. We ll discuss how we can help each other on our journey together. Here are our contact details / Send us a text message on XXX / Connect with me on LinkedIn. Who we are and what we believe in We are committed to shaping the future landscape of efficient, safe, and sustainable transport solutions. Fulfilling our mission creates countless career opportunities for talents across the group s leading brands and entities. Applying to this job offers you the opportunity to join Volvo Group . Every day, you will be working with some of the sharpest and most creative brains in our field to be able to leave our society in better shape for the next generation. We are passionate about what we do, and we thrive on teamwork. We are almost 100, 000 people united around the world by a culture of care, inclusiveness, and empowerment. Group Trucks Technology are seeking talents to help design sustainable transportation solutions for the future. As part of our team, you ll help us by engineering exciting next-gen technologies and contribute to projects that determine new, sustainable solutions. Bring your love of developing systems, working collaboratively, and your advanced skills to a place where you can make an impact. Join our design shift that leaves society in good shape for the next generation. Job Title: Specialist Simulation Engineer Durability Job Summary: We are looking for a highly skilled and self-driven CAE Simulation Engineer to join our Cabin Engineering team with a primary focus on durability simulations . This role involves leading advanced simulation activities, delivering engineering insights to support robust design decisions, and contributing to digital transformation within product development. Key Responsibilities: Ensure simulation accuracy and reliability by applying best practices, validated assumptions, and appropriate modelling simplifications. Develop and lead the implementation of robust, durable design solutions that meet performance targets across multiple disciplines. Conduct and lead linear, non-linear, modal, and transient structural simulations at both vehicle and subsystem levels. Perform fatigue life predictions and durability analyses using industry-leading fatigue analysis tools. Lead design optimization studies focused on weight, cost, and performance, while promoting the standardization of tools and methodologies. Contribute to the GTT Digital Transformation Simulation Subgroups , proposing and deploying new simulation methodologies. Correlate simulation results with physical test data to improve accuracy and support data-driven design validation. Work collaboratively across global teams throughout the entire product development lifecycle. Leverage data analytics to extract insights, refine simulation fidelity, and influence key design decisions in the durability domain. Exposure to scripting and automation tools is highly desirable. Soft Skills: Strong sense of ownership and accountability for quality, timeliness, and performance of all durability simulation deliverables from the GTT Bangalore team. Excellent communication skills, fast learner, team-oriented mindset, and a methodical approach to solving complex engineering problems. Qualifications: Masters degree in Mechanical Engineering , Automotive Engineering , or a related field. Required Experience & Skills: Minimum 12 years of CAE experience in the automotive industry, with a focus on product development and durability. Proven experience leading full lifecycle durability simulation programs across at least four major vehicle platforms. In-depth understanding of fatigue mechanics , material non-linearity , and advanced structural simulation techniques. Proficiency in tools such as MSC Nastran, ABAQUS, HyperWorks, nCode (or equivalent), and Beta-CAE . Experience with optimization techniques for mass and cost efficiency in engineering designs. Familiarity with physical testing , test-simulation correlation , and validation processes is a plus. Innovation-driven, with a history of filed patents and implementation of industrialized solutions. Authorship of technical publications or conference presentations is highly valued. Strong collaboration skills, attention to detail, and a proactive approach to continuous improvement.

Job Description (Meshing): Role: • Understanding the client’s design and analysis requirements. • Giving estimates to the designer/client. • Meshing the models in Hypermesh and setting decks for Optistruct. Required Skills: • The candidate should have 3 – 5 years of hands on experience on Hypermesh. • Should have worked on Heavy equipment structural domain. • The candidate should be in a position to work independently with minimum guidance from the team lead. • Giving estimates to the designer/client. Desired Skills: • Good written and oral communication skills. • Experience in Rail Transportation /Aerospace/Automotive/Heavy Engineering. Experience in analysis by using Optistruct solver. Education Qualification: B.E/B.Tech., in Mechanical Engineering with atleast 60% of marks.

Exposure to Aero Repairs/Concession Activities Proficiency in MS Office (Word, Excel, PPT) Hands-on experience with Tools NASTRAN, PATRAN & ISAMI Education Requirements BE / MTech in Aerospace or Mechanical Engineering Skills Required to Succeed in This Job Experience in Aero-structure, preferably with wing and high-lift devices Knowledge of concession treatment process Ability to provide stress assessment for various manufacturing non-conformities Strong knowledge in Strength of Materials, Aircraft Materials, and stress justification using hand calculations (classical methods) Experience working on AIRBUS A350 or legacy programs Familiarity with AIRBUS concession processes and methods Knowledge of AIRBUS-specific tools like ISAMI Experience with SAP PR3/PAC Fatigue and Damage Tolerance experience is an added advantage Able to meet tight deadlines and handle customer demands Willing to work early or late shifts based on project needs

As a Brake & Suspension CAE Analysis professional, your role involves preparing finite element models of Vehicle Chassis components and subsystems, with a focus on Brake, Suspension & Steering systems. You will be responsible for applying loading and boundary conditions for structural, thermal, and modal analysis of chassis parts, particularly brakes. Your duties include conducting CAE Analysis, correlating results with actual tests, interpreting results, and preparing detailed analysis reports. Your key responsibilities also include efficiently executing CAE activities for model development, Value Enhancement, and Quality resolution projects at various product development stages. You will participate in troubleshooting problems, analyzing issues, proposing countermeasures, and supporting their implementation. Additionally, you will assist the design team in generating and evaluating weight and cost reduction proposals and contribute to the improvement and development of CAE methodology. To excel in this role, you should possess a strong technical understanding of Chassis parts and subsystems, with a focus on brakes. You are expected to have the ability to perform virtual validation by interpreting physical test conditions. Proficiency in Noise and Vibration, Fatigue & Theory of Elasticity is essential. You should have a solid grasp of FEA, analysis at part, sub-system, and vehicle levels, as well as experience with tools like Hypermesh, Hyperview, Estech Sequal, ABAQUS, and NVH analysis using MSC Nastran. Desired qualifications include experience in Brake parts NVH, Structural CAE, and knowledge of Suspension & Steering CAE. In addition to technical skills, you are required to demonstrate good analytical ability, effective communication and presentation skills, problem-solving capabilities, an achievement-oriented mindset, teamwork skills, and networking abilities.,

You will be responsible for conducting Brake & Suspension CAE Analysis focusing on Strength, Durability, and NVH aspects. This will involve preparing finite element models of Vehicle Chassis components including Brake, Suspension, and Steering subsystems. You will apply loading and boundary conditions for structural, thermal, and modal analysis, with a specific emphasis on brake components. Your tasks will include conducting CAE Analysis, correlating results with actual tests, interpreting results, and preparing detailed analysis reports. Efficient execution of CAE activities for model development, Value Enhancement, and Quality resolution projects at various product development stages will be a key part of your role. You will participate in troubleshooting, propose countermeasures, and support their implementation. Additionally, you will assist the design team in generating and evaluating weight and cost reduction proposals. Your support in improving and developing CAE methodology will also be expected. In terms of technical competencies, you are required to have a good understanding of the functioning and design of Chassis parts, especially brakes. You should be capable of performing virtual validation by interpreting physical test conditions. Knowledge of Noise and Vibration, Fatigue, and Theory of Elasticity is essential. Proficiency in FEA, analysis at part, sub-system, and vehicle levels, as well as experience with tools like Hypermesh, Hyperview, Estech Sequal, ABAQUS, and Solver MSC Nastran for NVH analysis, will be advantageous. Desired qualifications include experience in Brake parts NVH, Structural CAE, and familiarity with Suspension & Steering CAE. On the behavioral side, you should possess strong analytical abilities, effective communication and presentation skills, problem-solving skills, a goal-oriented mindset, active team player qualities, and good networking skills.,

The FE Analyst will play a critical role in supporting the Product Design & Development team by conducting finite element analysis (FEA)) on a range of products, including industrial cranes, military vehicles, and construction equipment.

Conduct independent structural analysis (static & F&DT) on fuselage primary structures (PSE). Validate FEMs, extract loads, and ensure compliance with Airbus methods. Perform DMU cleaning, GFEM updates, and FEM validations. Apply mesh refinement rules for stress analyses (0D/1D/2D/3D). Extract & apply loads using Airbus in-house tools. Conduct hand calculations, Static Stress, Perform fatigue life calculations and crack growth Analyze composite/metallic materials for damage tolerance. Use ISAMI, HyperWorks suite (Hypermesh/View), MSC Nastran/Patran. Develop Excel VBA macros for automation. Contribute to Airframe certification tasks as needed. Requirements: bachelors/masters in Aerospace/Mechanical Engineering. 1-3 years of structural analysis experience (aircraft fuselage preferred). Proficiency in F&DT, FEM validation, and stress hand calcs. Strong skills in ISAMI, Hypermesh, MSC-NASTRAN/PATRAN, Airbus load tools. Experience with composite and metallic material behavior. Advanced Excel/VBA for data processing. Familiar with Aerospace certification requirements and processes. Preferred: A350XWB certification experience. Knowledge of Airbus design practices and PSE requirements