651 Abaqus Jobs - Page 3

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 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 27/29CS/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/ 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. 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 Qualification 15 years full time education.

Location: Bengaluru About us: We are a deep tech startup focusing on the development of aero engines and turbines for defence and energy applications. We are a dynamic team of aerospace enthusiasts. We are a passionate group focusing on scientific first principles based analysis and development followed by rapid hardware iterations. This is a fast paced work environment and demands quick execution and tangible results in a short period of time. Responsibilities: Perform structural analysis of aero engine components and rapid design iterations as part of a fast-paced dynamic team Perform calculations and analysis for loads, static and dynamic stresses, fatigue & creep. Go through rapid design and hardware iterations to develop critical hot section components Collaborate with other team members and account for interdependencies on other components Carry out modal analysis of rotary components Assist in carrying out vibration experiments, analysing data and Collaborate with propulsion, aerodynamicists and material engineers to optimize designs for high-temperature and high-stress environments. Qualifications: Understanding of aero engines and critical parts Bachelor&aposs degree in aerospace or mechanical engineering; master&aposs preferred. 2 - 3 years of experience in structural design and analysis. Proficiency in structural analysis software (e.g., ANSYS, Abaqus) Proficiency in first principles based analytical calculations and modeling Understanding heat treatment processes, standards and best practices Understanding of materials/super alloys for high temperature conditions Show more Show less

hackajob is collaborating with Boeing to connect them with exceptional tech professionals for this role. Overview As a leading global aerospace company, Boeing develops, manufactures and services commercial airplanes, defense products and space systems for customers in more than 150 countries. As a top U.S. exporter, the company leverages the talents of a global supplier base to advance economic opportunity, sustainability and community impact. Boeing’s team is committed to innovating for the future, leading with sustainability, and cultivating a culture based on the company’s core values of safety, quality and integrity. Technology for today and tomorrow The Boeing India Engineering & Technology Center (BIETC) is a 5500+ engineering workforce that contributes to global aerospace growth. Our engineers deliver cutting-edge R&D, innovation, and highquality engineering work in global markets, and leverage new-age technologies such as AI/ML, IIoT, Cloud, Model-Based Engineering, and Additive Manufacturing, shaping the future of aerospace. People-driven culture At Boeing, we believe creativity and innovation thrives when every employee is trusted, empowered, and has the flexibility to choose, grow, learn, and explore. We offer variable arrangements depending upon business and customer needs, and professional pursuits that offer greater flexibility in the way our people work. We also believe that collaboration, frequent team engagements, and face-to-face meetings bring together different perspectives and thoughts - enabling every voice to be heard and every perspective to be respected. No matter where or how our teammates work, we are committed to positively shaping people’s careers and being thoughtful about employee wellbeing. With us, you can create and contribute to what matters most in your career, community, country, and world. Join us in powering the progress of global aerospace. Position Overview Boeing India Engineering is looking for Experienced Structural Analysis Engineer (Service Engineering) to support Airframe Service Engineering Capability at Boeing India, Bangalore. This position will focus on providing 24/7 support to Boeing commercial airplane customers. This position offers a unique opportunity to work complex technical challenges in support of safety operation and return to service. Our team of engineers support over 14,000 aircraft around the globe, and work closely with our customers to ensure that their fleet is operating safely, efficiently, and reliably. Join us today and help shape the future of commercial aviation Position Responsibilities: Primary responsibilities for this position include: Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as an integrated team Responsible to collaborate with Service Engineers to perform root cause analysis and corrective actions on Sin-Service issues for Airframe and other Mechanical systems. Performs detailed structural analysis (static strength, durability/fatigue and damage tolerance) to determine structural integrity (margins of safety), using classical techniques and Boeing tools. Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method Generate documentation to report analysis and test results to support certification/Qualification Support Gated Reviews to validate the quality and completeness of work packages Familiar with regulatory framework (FAA and Mil-Spec), for warranting safety and regulatory compliance. Guides structural design and configuration development. Supports in-service products by investigating failures and analyzing improvements Performs trade studies to optimize structure and meet program requirements. Researches and prepares data to support definition of structural design requirements. Willing to support a 24/7 on-call rotation schedule and the ability to work variable shifts, including weekends or overtime. Basic Qualifications (Required Skills/Experience): Bachelor’s or Master’s degree is required as a basic qualification in Mechanical/Aerospace/Applied Mechanics/Structural engineering 9 to 12 years of proven experience in stress analysis in Services related to Fleet Support. Preferred Qualifications (Desired Skills/Experience): Experience in structural analysis of various airframe structures. Experience of Aircraft maintenance and service procedures Experience with structural analysis of metallic and composite structures. Experience with static, fatigue and damage tolerance analysis Knowledge of airplane operating environments Robust understanding of engineering fundamentals such as material properties, Free-body diagrams, structural loads and analysis methods Experience in utilizing FEM software (e.g., ABAQUS, PATRAN/NASTRAN, Hyperworks) Experience or training with computer programming languages (e.g., Matlab, Python, Visual Basic) Experience in utilizing industry CAD systems (e.g., NX/Teamcenter and CATIA/ENOVIA) Candidate demonstrates excellent analytical and problem-solving skills Good verbal and written communication skills to liaise with several Stakeholders Ability to work across functional teams and organizations Willingness to expand into technical areas without prior experience Desire to continuously improve our airplanes Typical Education & Experience: Typical 9 to 12 years of related work experience. Advanced degree (e.g. Bachelor, Master, etc.) preferred.

🔹 We’re Hiring: Technical FEA Support Engineer (RoboAnalyzer & FEAST FEA) 📍 Pune, Maharashtra, India (Hybrid) | 🏢 SVR Robotics Pvt. Ltd. | 🕑 1–2 years experience (exceptional freshers welcome) 🚀 About the Role Do you enjoy solving real-world engineering problems with simulation? At SVR Robotics , we’re looking for a hands-on engineer who will be the go-to technical expert for RoboAnalyzer (robot kinematics/dynamics) and FEAST FEA (structural/thermal/modal/buckling). You’ll support educators, researchers, and industry users in modeling, analyzing, troubleshooting, and achieving accurate results—fast. 💡 What You’ll Do Provide Level-1 & Level-2 technical support : reproduce issues, debug models, suggest fixes/workarounds. Build & validate FEA models: geometry cleanup, meshing, BCs/loads, nonlinear/contact setups, solver runs, and post-processing. Develop tutorials, guides, and example models (videos + documentation) for users. Conduct trainings, webinars, and lab sessions for colleges and customers. Support POCs/benchmarks, capture product feedback, and maintain knowledge base/FAQ. Advise on installation, licensing, and environment setup (Windows/Linux). Enable workflows between RoboAnalyzer → FEAST studies with validation & reporting. Track KPIs: response/resolution times, CSAT, training NPS, tutorial usage, renewal/POC conversions. 🎓 Must-Have Skills B.E./B.Tech (Mechanical/Aerospace/Mechatronics) or M.Tech in a related field. Strong fundamentals: strength of materials, vibrations, FEM basics, heat transfer . 1–4 yrs in FEA toolchain (FEAST/ANSYS/Abaqus/Nastran/CalculiX, etc.) or strong project work as fresher. Proficiency in meshing, contacts, nonlinear/materials, convergence, results interpretation & report writing . Strong communication skills; comfortable with customer demos/trainings. Fluency in English (Hindi/Marathi a plus). 🌟 Good to Have Hands-on with FEA modules (static, modal, buckling, thermal, nonlinear) and RoboAnalyzer . Python/MATLAB scripting for automation & post-processing. CAD familiarity (SolidWorks/Creo/CATIA); experience with Git/Jira/Confluence/Notion. Exposure to robotics (manipulator arms, Stewart platform dynamics) & HPC/parallel runs. ✨ Why Join Us? Work on cutting-edge FEA & robotics tools shaping education and industry. Hybrid work environment (Pune-based). Direct exposure to customers, developers, and product innovation . Growth-focused culture with training opportunities. 👉 Interested? Apply now by sending your CV to admin@svrrobotics.com or connect with us here on LinkedIn. #Hiring #FEA #EngineeringJobs #Robotics #Simulation #RoboAnalyzer #FEASTFEA #MechanicalEngineering #AerospaceEngineering #Mechatronics #FEM #PuneJobs #TechCareers #SVRRobotics

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

Job Requirements A Civil and Structural Design Engineer in the oil and gas industry is a highly specialized professional responsible for the end-to-end design, analysis, and integrity management of complex facilities. This role covers initial conceptual studies to detailed engineering, and ongoing operational support for both greenfield and brownfield projects. The engineer ensures the safety, cost-effectiveness, and structural soundness of all civil and structural assets, whether on land or offshore. A deep understanding of industry-specific codes and standards is critical to ensure compliance and mitigate high-risk scenarios. Key roles and responsibilities Design and engineering Perform advanced structural analysis and design for both reinforced concrete and steel structures, including pipe racks, platforms, foundations, and buildings. Design specialized foundations, such as dynamic foundations for large rotating machinery, and pile foundations for complex structures. Conduct comprehensive in-place, fatigue, seismic, and blast analysis for both onshore and offshore structures. Develop detailed engineering deliverables, including technical specifications, calculation reports, and engineering drawings (GAs, details, layouts). Utilize advanced engineering software (e.g., STAAD.Pro, SACS, ABAQUS, Navisworks) for structural analysis, simulation, and 3D modeling. Project management and coordination Lead the civil and structural aspects of projects from the conceptual (FEED) stage through detailed design and into execution. Collaborate with other engineering disciplines (process, piping, mechanical, electrical) to ensure seamless integration of designs. Perform clash detection and resolution using 3D modeling tools to identify and mitigate conflicts with other disciplines. Provide technical support to the procurement process by reviewing vendor bids and material requisitions. Manage project schedules, budgets, and change requests related to the civil/structural scope of work. Integrity and maintenance Conduct structural integrity assessments of existing facilities, performing fitness-for-service evaluations. Develop and implement structural inspection and reliability programs to monitor the health of assets. Provide technical support and repair recommendations for in-service structures based on inspection reports and risk assessments. Support decommissioning projects by designing removal and demolition procedures. Field and construction support Perform site visits and inspections to ensure construction activities comply with design specifications. Provide on-site technical guidance, address construction queries, and evaluate change orders. Develop installation aids and construction methodology, especially for offshore components. Support in Turnaround Engineering with Construction and Temporary support arrangements and necessary calculations in both Upstream and Refinery facilities Documentation and quality assurance Ensure all designs and deliverables comply with strict international and industry-specific standards, such as API, AISC, Eurocodes, and relevant environmental regulations. Maintain accurate and organized project documentation, including design changes and revision controls. Oversee quality control of contractor and vendor work throughout the project Work Experience Required skills and qualifications Education and experience Education: Bachelor&aposs or Master&aposs degree in Civil or Structural Engineering. Experience: 8-12 years of relevant experience in a high-risk industry, preferably in oil and gas, petrochemicals, or energy. Project Experience: Proven experience in both greenfield and brownfield projects, covering all project phases from FEED to commissioning. Technical expertise Analysis and Design: Expertise in the design of complex structures (concrete and steel), dynamic analysis of equipment foundations, fatigue, seismic, and blast-resistant design. Codes and Standards: In-depth knowledge of international codes, including API (2A, 1104, etc.), AISC, ASME, and other relevant standards. Software Proficiency: Advanced user of structural analysis and design software such as STAAD.Pro, SACS, ABAQUS, or ANSYS. Modeling Tools: Experience with 3D modeling and review software, including Tekla, Navisworks, or E3D. Personal and interpersonal skills Analytical Skills: Strong analytical and problem-solving abilities with meticulous attention to detail. Communication: Excellent verbal and written communication skills to articulate complex technical issues to multidisciplinary teams and clients. Teamwork: Ability to work effectively within an integrated team environment and collaborate with multiple stakeholders. Leadership: Proven ability to lead design teams and mentor junior engineers 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 : 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/ OptistructLS 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 Qualification 15 years full time education

Overview This role is a technical lead role within ICC, Hyderabad that will co-ordinate with Data Science and Analytics team on creation of new digital capabilities and sustaining existing digital capabilities. This role will act as the key technical expert dedicated to Foods Packaging Modeling & Simulation development (70%). This role also has the managerial responsibility of leading all DSA-ICC associates (30%). This role will act as one of the key technical specialists for packaging modeling & simulation. This role also will serve as local simulation team Lead to drive overall deliverables. The role will be responsible for performing simulations using FEM, DEM, CFD and other techniques and providing insights that influence the design and development of R&D applications, with focus on Foods Packaging applications. This role will also Collaborate with internal and external stakeholders in a global setting and will support Troubleshooting & Problem Solving to Diagnose and resolve issues related to simulation models and results. This role also is responsible for developing 3DX Apps, Graphical User Interfaces (GUI) and simulation templates. This role will also provide leadership to all simulation and modelling teams ( including other associates ). Responsibilities Lead a team of Modelling, Simulation and other SMES of DSA team ( Including Bev Pkgs Teams) based out of Hyderabad. Provide Strategic direction in alignment with global teams and ensure timely delivery of Committed projects. Functional Responsibilities Deliver Foods Packaging Simulation models and apps per Simulation Roadmap and Timeline above Deliver modeling and simulation projects using 3DX, other general purpose and specialized numerical software. Collaborate with Dassault experts directly on delivering perfect packaging simulation templates and apps Design and develop innovative experiments to validate and improve models. Support other senior simulation engineers on assigned simulation tasks including CAD creation, CAD cleaning, meshing, pre-processing, post processing, creating visuals of data Work with external partners, software vendor, university, engineering firms, to develop technologies needed to fulfil PepsiCo need. Additional responsibilities in combining physics-based simulation, sensor technology, data analytics (AI/ML) to deliver digitized innovation projects (digital twin), Support Computational Chemistry projects by data collection and literature research New technology introduction and implementation Qualifications PhD. with simulation concentration and 8+ years of work experience, MS with 10+ years experience Background in mechanical engineering, solid mechanics or related field Packaging experience with cardboard boxes, films, pallets, is a big plus but not necessary Hands-on experience with commercial software - CFD (ANSYS FLUENT, STAR-CCM+), FEA (ABAQUS, ANSYS Mechanical), DEM (ROCKY, EDEM), COMSOL. Knowledge about computational chemistry (hands on software experience with MOE, Shrodinger a plus) Experience designing and conducting physical testing required to formulate and/or calibrate models, i.e., Wind tunnel, mechanical testing, thermal measurements, Data Acquisition, High speed imagery, etc. Experience with Python, MATLAB, R, JMP a plus. Experience with VR/AR assets creation using KeyShot, Unity, Unreal, or Omniverse a plus. Knowledge and experience in food/beverage production and process engineering a plus extrusion, drying, frying, mixing, filling, food safety. Strong project management and communication skills. Ability to collaborate with internal and external partners in a global setup. Robust understanding of engineering principle with experience in the area of fluid dynamics, thermodynamics and heat transfer. Experience with state-of-the-art modeling software that capable to model multi-physics problem involving multi-phase fluid flow and heat transfer in engineering and manufacturing processes. Knowledge of how to use simulation to evaluate new and novel technologies for PepsiCo s innovation in processing/packaging. PhD. with simulation concentration and 8+ years of work experience, MS with 10+ years experience Background in mechanical engineering, solid mechanics or related field Packaging experience with cardboard boxes, films, pallets, is a big plus but not necessary Hands-on experience with commercial software - CFD (ANSYS FLUENT, STAR-CCM+), FEA (ABAQUS, ANSYS Mechanical), DEM (ROCKY, EDEM), COMSOL. Knowledge about computational chemistry (hands on software experience with MOE, Shrodinger a plus) Experience designing and conducting physical testing required to formulate and/or calibrate models, i.e., Wind tunnel, mechanical testing, thermal measurements, Data Acquisition, High speed imagery, etc. Experience with Python, MATLAB, R, JMP a plus. Experience with VR/AR assets creation using KeyShot, Unity, Unreal, or Omniverse a plus. Knowledge and experience in food/beverage production and process engineering a plus extrusion, drying, frying, mixing, filling, food safety. Strong project management and communication skills. Ability to collaborate with internal and external partners in a global setup. Robust understanding of engineering principle with experience in the area of fluid dynamics, thermodynamics and heat transfer. Experience with state-of-the-art modeling software that capable to model multi-physics problem involving multi-phase fluid flow and heat transfer in engineering and manufacturing processes. Knowledge of how to use simulation to evaluate new and novel technologies for PepsiCo s innovation in processing/packaging. Lead a team of Modelling, Simulation and other SMES of DSA team ( Including Bev Pkgs Teams) based out of Hyderabad. Provide Strategic direction in alignment with global teams and ensure timely delivery of Committed projects. Functional Responsibilities Deliver Foods Packaging Simulation models and apps per Simulation Roadmap and Timeline above Deliver modeling and simulation projects using 3DX, other general purpose and specialized numerical software. Collaborate with Dassault experts directly on delivering perfect packaging simulation templates and apps Design and develop innovative experiments to validate and improve models. Support other senior simulation engineers on assigned simulation tasks including CAD creation, CAD cleaning, meshing, pre-processing, post processing, creating visuals of data Work with external partners, software vendor, university, engineering firms, to develop technologies needed to fulfil PepsiCo need. Additional responsibilities in combining physics-based simulation, sensor technology, data analytics (AI/ML) to deliver digitized innovation projects (digital twin), Support Computational Chemistry projects by data collection and literature research New technology introduction and implementation

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 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 27/29CS/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/ 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. 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 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

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 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 27/29CS/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/ 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. 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 Qualification 15 years full time education

Experience: 3 years to 5 Years Category: zINACTIVE - Information Technology Main location: Bangalore Employment Type: Full Time Job Description: - AI-ML Engineer We are seeking a high-impact AI/ML Software Engineer to join our AI engineering team. The ideal candidate brings deep expertise in modern agentic frameworks such as Google ADK, CrewAI, AutoGen, or LangGraph, and hands-on experience in developing Model Context Protocols (MCP). This role is ideal for individuals passionate about engineering through automation, scaling AI architecture, and contributing to the next generation of agent-based systems. You will work closely with our CICD platform tooling and global architecture teams to enhance and productize our agentic SDLC platform. Key Responsibilities: Design, develop, and maintain Kubernetes-based containerized microservices and CICD automation pipelines that support SDLC. Build modular agent workflows capable of reasoning, collaborating, and adapting dynamically to context and goals. Develop and manage multi-agent systems using frameworks like Google ADK, CrewAI, or AutoGen. Build and optimize MCP pipelines, including context injection, memory caching, semantic retrieval, and embedding-based context scoping. Develop CLIs and SDKs to support MCP testing and integration. Collaborate with cross-functional teams including product, data analytics, and infrastructure to evolve tooling for agent development, prompt evaluation, and telemetry analysis. Fine-tune foundation models (e.g., GPT, Claude, Falcon) for enhanced domain-specific performance. Required Qualifications: Bachelors degree in computer science, Engineering, Mathematics, or a related technical field. 25 years of software engineering experience, with at least 2 years focused on AI/ML or developer platform teams. Strong coding skills in Python and Golang, with a track record of writing clean, secure, and scalable code. Proven experience in MCP implementation, ensuring efficient, coherent, and context-aware data flow in multi-agent LLM systems. Experience with Kubernetes, service mesh technologies (e.g., Istio), and Infrastructure-as-Code (IaC). Familiarity with distributed task orchestration and real-time agent execution environments. Skills: Artificial Intelligence Kubernetes

Job Description Summary As Senior Engineer Design Tools & Methods you will own, maintain and enhance inhouse design tools for GEV wind business needs. In this role, you will be responsible for improvising blade design quality through maintenance of and creation of new features in our in-house blade design tool, LMBlades and/or CATIA automations. Further, as senior engineer, you are expected to build programming expertise of in-house applications and ensure wing to wing ownership including user empowerment for the new tools or features developed by you. Job Description Roles and Responsibilities Own, maintain & simplify wind blade modelling softwares (LMBlades & CATIA) by leveraging existing developments and simplifying it for GEV wind business needs. Ownership & maintenance of various automation features of LMBlades & CATIA based customized tools. Leverage & develop web-based process for databases to enable single design model platform for all needs and thus avoid fidelity differences & user errors of maintaining multiple models. Leverage LMB internal program features for quick blade cross-section, span view, basic calculations etc. Integrate beam level fatigue assessments based out of FEA strains for faster evaluations. Develop beam model creation process in alignment with LMBlades and systems input need of validated beam model. Develop alternatives for dependent features which are critical for program. Ensure seamless and efficient integration to CATFEM process. Mentor young programmers for effective development and deployment of new tool features. Empower and guide users to help debug and resolve issues. Required Qualifications Bachelors degree in mechanical, aerospace, composite or civil structural engineering 10-12 years of experience in software development for mechanical structure application including software deployment skills. Experience in programming languages C++, C#, VBA & Python and Finite Element Analysis & simulation tools such as CATIA, ABAQUS/ ANSYS. Proactive, well organized, self-motivated, able to work and complete tasks independently and on time. Focus on possibilities rather than limitations. Excellent communication, interpersonal and presentation skills Proven experience with design tools creation, deployment and user empowerment. Leadership skills with proven ability to handle multiple task/people and obtain effective project outcome. Ability to influence & build consensus with cross functional team & stakeholders. Desired Characteristics Post graduate degree from an accredited university or college in Mechanical Engineering, Aerospace Engineering, Engineering Mechanics, or equivalent. Strong technical expertise in wind turbine blade composite structure with demonstrated ability to design and own engineering outcomes regarding safety, quality, and fulfilment of customer needs. Good knowledge about CATIA customization using CAA API. Experience in CATIA CAA & VBA programming including OOPS (object-oriented programming) Knowledge of wind turbine rotor blade full scale manufacturing and component level process trials Demonstrated communication and interpersonal skills, with the ability to communicate complex technical concepts clearly and concisely to individuals at all levels of the organization while ensuring transparency and gaining alignment with internal/external stakeholders. Proven track record of curiosity and a strong passion for identifying and turning new ideas, technologies, and methodologies into product differentiated outcomes. Experience with coaching, mentoring, and developing technical engineering talent to guide their professional growth and career advancement in tools/methods development.

The Intern will be working on Structural problems using Finite Element Analyses. They will be guided on FEA methodologies and different analysis approach, preprocessing techniques and application of fundamental physics to real world challenges. Expecting the intern to be proficient in Machine Design and Engineering Mechanics. Primary tools used will be Abaqus CAE, Altair HyperMesh Position Intern, FEA Location IND, Bangalore, KA How Youll Create Possibilities Role Responsibilities : Learn fundamentals of FEA, the software and apply learnings to get a good firsthand experience in FE simulations. Support in the setup and execution of FEA simulations using commercial software (e.g., Abaqus, HyperMesh). Prepare parts and sub system for analysis, post process the model and support analysis of details. Contribute to the development and optimization of simulation models to enhance accuracy and efficiency. Contributes to the creation of CAD geometries and meshing for FEA models. Use simulation methods to create structural models, apply loads and boundary conditions, and predict structural response of the FEA models Prepare clear and concise reports, presentations, and documentation of simulation work. What Youll Bring to Our Team Qualifications : A student from final year M. Tech or one who has completed M. Tech in Mechanical Engineering with specialization in Machine Design, Engineering Mechanics and FEM. Excellent oral and written communication skills. A passion for technology and appetite to learn new things with limited guidance. Firsthand experience in MS office & visualization of engineering drawings Experience in Creo/ HyperMesh/ Abaqus will be a plus. Skills & Attributes Strong visualization skills to interpret problem statements, drawings, and figures accurately. Experience with meshing tools (HyperMesh or Abaqus meshing capabilities) Programming skills (e.g., Python) for scripting and automation. Familiarity with High-Performance Computing (HPC) environments. Prior project experience involving FEA (academic or personal).

Career Area: Engineering Job Description: Your Work Shapes the World at Caterpillar Inc. When you join Caterpillar, youre joining a global team who cares not just about the work we do but also about each other. We are the makers, problem solvers, and future world builders who are creating stronger, more sustainable communities. We dont just talk about progress and innovation here we make it happen, with our customers, where we work and live. Together, we are building a better world, so we can all enjoy living in it. Role Definition Solve challenging engineering problems involving products, systems, and components using advanced simulation techniques and analysis. Responsibilities Collaborate with customers and leadership to scope and execute projects that meet the needs of the business. Experience as an individual contributor in performing complex validation projects/programs, technical coaching/mentoring other team members Degree Requirement Degree required Post Graduate / Ph. D degree from a reputed institution, in an accredited Engineering curriculum (Mechanical / Design / Automobile / Aerospace) and 2 + years of industry experience. Skill Descriptors Technical Excellence : Knowledge of a given technology and various application methods; ability to develop and provide solutions to significant technical challenges. Level Basic Understanding: Structural durability of turbomachinery/diesel engine systems Sound understanding of principles of HCF/LCF, thermals and vibrations Problem Solving: Knowledge of approaches, tools, techniques for recognizing, anticipating, and resolving organizational, operational or process problems; ability to apply knowledge of problem solving appropriately to diverse situations. Level Working Knowledge: Demonstrated excellent judgement and decision-making ability Demonstrated ability to independently solve problems Excellent analytical skills and the ability to perform complex task Computer-Aided Design & Engineering: Knowledge of tools and techniques of specialized graphics programs; ability to produce, analyze, simulate and test product design drafts. Level Working Knowledge: Expertise in using FEA tools like ANSYS/ABAQUS etc for solving complex non-linear FEA, Multiphysics simulations related to structural LCF/HCF. Effective Communications: Understanding of effective communication concepts, tools and techniques; ability to effectively transmit, receive, and accurately interpret ideas, information, and needs through the application of appropriate communication behaviors. Level Working Knowledge: Must have ability to communicate technical information effectively with team members and others in the work group Excellent Teamwork and collaboration skills Relocation is available for this position.

Satyam Ventures hiring Onsite - (NVH + Durability) Analysis Engineer Job Location: Michigan & California Visa Validity : H1B(Mandatory) Experience: 8 to 13 Years Qualification B.E/M.E (Automotive, Mechanical) Skill Set: Abaqus, Nastran, Optistruct, Hypermesh, Ansa, Hyperview, Metapost Notice Period: Immediate to 30 days only. Job Description: Strong fundamentals of Nonlinear FEA, Optimization for strength and stiffness targets. Fatigue life estimations for parent metal and weld connections. Strong fundamentals of Structural dynamics, Modal analysis and dynamic responses (FRF and Random excitations). Full vehicle level NVH studies with point mobility and local dynamic stiffness expertise and optimizations for target frequencies and dynamic responses. Intuitive understanding of structural mechanics and problem-solving attitude to come up with countermeasures with manufacturing and assembly feasibility. Exposure to Multi-Body dynamics simulations with flex-body analysis is welcome. Interested candidates can share their profiles to Vasavadathu_Taticherla@satven.com.

About The Role Skill required: User-Generated Content Moderation - Content Moderation Designation: Trust & Safety New Associate Qualifications: Any Graduation Years of Experience: 0 to 1 years What would you do? You will be responsible for analyzing and reviewing user profiles, audio, videos, and text-based content and/or investigating, escalating and/or resolving issues that are reported by users or flagged by the system. Due to the nature of the role, the individual may be exposed to flashing lights or contrasting light and dark patterns.Identify the spam content to provide genuine search results. Help the victims to remove their explicit videos / Photographs from global sites. Remove the Personal Identifiable information reported by the user from various search results. Addressing ad blocking through improving ad experiences across the web.Content moderation is meaningful work that helps keep the internet safe. It may also be challenging, at times. In the context of this role, individuals may be directly or inadvertently exposed to potentially objectionable and sensitive content (e.g., graphic, violent, sexual, or egregious). Therefore, content moderators need strong resilience and coping skills. We care for the health and well-being of our people and provide the support and resources needed to perform their role responsibilities. Active participation in Accentures well-being support program, designed specifically for the Trust & Safety community, provides valuable skills to promote individual and collective well-being. What are we looking for? Adaptable and flexibleAbility to perform under pressureAbility to handle disputesAbility to meet deadlines Roles and Responsibilities: In this role you are required to solve routine problems, largely through precedent and referral to general guidelines Your primary interaction is within your own team and your direct supervisor In this role you will be given detailed instructions on all tasks The decisions that you make impact your own work and are closely supervised You will be an individual contributor as a part of a team with a predetermined, narrow scope of work Please note that this role may require you to work in rotational shiftsReview, classify and/or remove content according to client guidelines, using specific tools and channelsUnderstand and remain updated on changing client policies and guidelinesInvestigate, resolve, and relay complex content issues to the broader Trust and Safety teamStrong coping, emotional resilience, and stress-management skillsExcellent comprehension, communication, and English skillsAbility to perform duties objectively, devoid of inherent biases or personal beliefs, in the best interest of client policiesStrong attention to detailComfort synthesizing and analyzing information from multiple streamsStrong critical thinking and decision-making skills Qualification Any Graduation

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 : Aircraft Design 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 and oversee the design and development of aircraft primary and secondary structures, guiding distributed teams across the program.Establish and govern engineering best practices, design review frameworks, and technical quality gates throughout the program lifecycle.Provide technical oversight for concept development, structural architecture, detailed design, integration, and certification phases.Ensure integration of cost, weight, design for manufacturability/assembly (DFM/DFA), and safety targets into structural design processes.Lead root cause investigations, risk assessments, and resolution strategies for design issues, non-conformances, and airworthiness deviations.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 lifecycle. 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. Represent engineering during customer technical audits, program quality gate reviews, and change control reviews. Ensure engineering activities meet cost, schedule, and performance objectives while maintaining traceability and compliance. Promote and institutionalize Model-Based Definition (MBD) and Model-Based Systems Engineering (MBSE) for traceability, digital twin integration, and requirement verification. Drive the adoption of systems thinking, ensuring structural designs align with broader system-level functional, interface, and safety requirements. Build and mentor a high-performance engineering team by setting technical vision, growth plans, and knowledge-sharing frameworks. Conduct structured technical coaching, performance reviews, and succession planning for key engineering roles. Contribute to internal competency development initiatives, including design automation, and workflow digitization. Professional & Technical Skills: In-depth understanding of aircraft load-bearing structures, with focus on structural integrity, stiffness, and load path optimization under both static and dynamic conditions. Strong awareness of stress analysis considerations, including fatigue, damage tolerance, and failure modes relevant to metallic and composite airframe components. Practical knowledge of production tooling design, jigs & fixtures, and their influence on design tolerances, datum schemes, and manufacturability. Familiar with 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 via PLM systems such as Teamcenter. Expertise in the design and integration of metallic, sheet metal, and composite aircraft structures for both primary and secondary components. Strong understanding of load path optimization, stress inputs, fatigue and damage tolerance, and design-for-certification. Familiarity with airworthiness regulations (e.g., CS-27/29, FAR 23/25), OEM design standards, and FAA/EASA certification processes. Advanced proficiency in Siemens NX, Teamcenter, and other PLM/PDM tools. Working knowledge of CATIA V5, VPM, or ENOVIA is a plus. Solid grasp of GD&T, ASME Y14.5, and industry drawing standards. Experience managing design-to-cost, design-to-weight, and sustainability considerations across the design lifecycle. Exposure to digital twin strategy, systems architecture alignment, and model validation in a systems-engineering context. Proficient in Siemens NX and Teamcenter is essential. Experience in CATIA V5, VPM, ENOVIA, or similar tools is a strong plus. Familiarity with digital engineering ecosystems, including MBD/MBSE implementation, PLM workflows, and engineering change management. Technically strong and solution-oriented, with the ability to guide teams through ambiguity and complexity. Proven experience in technical team leadership, task planning, design reviews, and decision-making across program phases. Strong communication and client engagement skills; able to articulate design rationale and negotiate technical outcomes with stakeholders. Committed to mentoring junior engineers and contributing to organizational knowledge development and delivery excellence. Strategic thinker with a continuous improvement mindset, especially in design quality, process optimization, and engineering best practices. Proven experience in 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, and qualitywithin complex delivery frameworks for aerostructure development programs. Additional certifications in project management (PMP/Prince2), Six Sigma, or Digital Engineering are advantageous. Additional Information:- The candidate should have a minimum of 15 years of experience in 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 and The role is strictly on-site and requires physical presence at the clients office in Bangalore..- A B Tech in Mechanical Engineering or Aerospace 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

About The Role Skill required: User-Generated Content Moderation - Content Moderation Designation: Trust & Safety Associate Qualifications: Any Graduation Years of Experience: 1 to 3 years Language - Ability: Burmese - Advanced What would you do? You will be responsible for analyzing and reviewing user profiles, audio, videos, and text-based content and/or investigating, escalating and/or resolving issues that are reported by users or flagged by the system. Due to the nature of the role, the individual may be exposed to flashing lights or contrasting light and dark patterns.Content moderation is meaningful work that helps keep the internet safe. It may also be challenging, at times. In the context of this role, individuals may be directly or inadvertently exposed to potentially objectionable and sensitive content (e.g., graphic, violent, sexual, or egregious). Therefore, content moderators need strong resilience and coping skills. We care for the health and well-being of our people and provide the support and resources needed to perform their role responsibilities. Active participation in Accentures well-being support program, designed specifically for the Trust & Safety community, provides valuable skills to promote individual and collective well-being. Reviewing of photos, videos, and text-based content and make judgments as to whether reviewed content is in violation of our Clients terms of services. The content may cover may be sensitive in nature. Ensuring every piece of content in violation of clients terms of services is accurately identified and flagged for action in a timely manner. What are we looking for? Review, classify and/or remove content according to client guidelines, using specific tools and channelsUnderstand and remain updated on changing client policies and guidelinesInvestigate, resolve, and relay complex content issues to the broader Trust and Safety teamStrong coping, emotional resilience, and stress-management skillsExcellent comprehension, communication, and (insert language) skillsAbility to perform duties objectively, devoid of inherent biases or personal beliefs, in the best interest of client policiesStrong attention to detailComfort synthesizing and analyzing information from multiple streamsStrong critical thinking and decision-making skills Roles and Responsibilities: In this role you are required to solve routine problems, largely through precedent and referral to general guidelines Your expected interactions are within your own team and direct supervisor You will be provided detailed to moderate level of instruction on daily work tasks and detailed instruction on new assignments The decisions that you make would impact your own work You will be an individual contributor as a part of a team, with a predetermined, focused scope of work Please note that this role may require you to work in rotational shifts Qualification Any Graduation