60 Patran Jobs - Page 2

As a Lead Consultant-FE Engineer at Genpact, you will play a crucial role in maintaining and creating tableau dashboards while ensuring data accuracy and resolving any report extraction issues. Your expertise in FE modelling using ANSYS (Workbench & APDL) and HYPERMESH, as well as experience in Static (Linear and Non-Linear) and Dynamic analysis, will be essential in analyzing various mechanical components and systems. Additionally, your knowledge of HCF/LCF fatigue analysis, composites, and fatigue analysis will be highly valued. Your responsibilities will include: - Demonstrating rich experience in FE modelling using ANSYS and HYPERMESH - Conducting Static (Linear and Non-Linear) and Dynamic analysis - Performing HCF/LCF fatigue analysis - Analyzing various mechanical components and systems - Possessing knowledge of Composites, Fatigue analysis (an added advantage) - Demonstrating good communication and presentation skills Qualifications we seek in you: - Minimum Qualification: BE in Mechanical Engineering or Equivalent Preferred Skills: - Knowledge in ABAQUS, Patran, Nastran If you are passionate about leveraging your skills in engineering, analysis, and communication to drive impactful outcomes, we invite you to join our team as a Lead Consultant-FE Engineer at Genpact.,

Greetings from HCLTech..! Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as an integrated team • Structural analysis includes calculation of loads, Static analysis, Fatigue analysis, Damage-Tolerance analysis, and Vibration analysis •Evaluate structural integrity of aircraft components by way of classical hand calculations and, finite element method •Generate documentation to report analysis results to support certification Basic Qualifications: •Bachelors or Masters in Mechanical/Aerospace engineering •5-10 years of relevant experience •Experience with structural analysis of metallic and composite various airframe structures • Experience is providing the Quality Notification Stress dispositions and well wersed with the repair methedologies •Experience with static and fatigue analysis •Robust understanding of engineering fundamentals such as material properties, Free-body diagrams, loads and, analysis methods • Experience in utilizing FEM software (e.g., PATRAN/NASTRAN, Hyperworks) •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

Overview 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): Bachelors or Masters degree is required as basic qualification in Mechanical/Aerospace/Applied Mechanics/Structural engineering along with 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.) required. Education Bachelor's Degree or Equivalent Required Shift Shift rotation - weekdays (India).

Project Role : Manufacturing Engineering Practitioner Project Role Description : Define processes to fabricate, assemble, inspect and test new products and machines based on production engineering and design principles. Define the supporting tools and fixtures needed for production. Develop procedures, product specifications and define the quality standards and inspection methods. Must have skills : Aircraft Structural Analysis Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications. The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as team lead (45 members) for structural analysis and stress evaluationsTechnical customer liaison; deliver training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisExpertise in specific tools/methodologies for the OEMStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:5-8 years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru Qualification 15 years full time education

Project Role : Manufacturing Engineering Practitioner Project Role Description : Define processes to fabricate, assemble, inspect and test new products and machines based on production engineering and design principles. Define the supporting tools and fixtures needed for production. Develop procedures, product specifications and define the quality standards and inspection methods. Must have skills : Aircraft Structural Analysis Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications. The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as team lead (45 members) for structural analysis and stress evaluationsTechnical customer liaison; deliver training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisExpertise in specific tools/methodologies for the OEMStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:5-8 years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru 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 : NAMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications.The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as key team member for structural analysis and stress evaluationsIndependent technical; deliveries, training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisExpertise in specific tools/methodologiesStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:2-5 years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru 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 : NAMinimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications. The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as SME and team lead (1015 members) for structural analysis and stress evaluationsTechnical customer liaison; deliver training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs, with strong expertise in OEM-specific tools and methodologies.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Skilled in leading and managing teams of 1015 engineers, ensuring project milestones and quality standards are met.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:8+ years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru Qualification 15 years full time education

Graduate/Postgraduate (Aerospace/Mechanical/Civil) Perform Fatigue and Damage Tolerance (F&DT) calculations of Aircraft Components (Fuselage, Wing, HT/VT) Perform Spectrum Generation added advantage Calculation of Equivalent Stress (Fatigue and Crack Propagation), Understanding of Mission Profiles, Rain flow counting, Miners Rules Calculation of Stress Concentration Factor (Kt) added advantage Knowledge of Static & Fatigue Design Values Good in Report writing added advantage Sound knowledge of Aircraft Loads and Structural Design Principles Background in Design & Sizing of Aircraft Primary and Secondary Structural Components Very good analytical and reasoning skills Experience MSC – Fatigue, MSC – Patran/Nastran, MSC – Marc, NASGRO, Hyper works, Franc 3D, MS Office Good communication & Interpersonal Skills Flexibility & Adaptability

Dear Candidate: Greetings from Metrics Numero Talent Acquisition Team!!! MetricsNumero was founded with the goal of creating a centre of excellence that provides high-quality services in Aerospace , Mechanical, SAP, Microsoft, AI/ML, EDW-BI & Data Analytics, Cloud services Mechanical Engineering & Design, ERP and Banking solutions to a wide range of industries globally. Our driving force is to provide innovative solutions to complex business problems. We are specialized in Software Advisory & Consultation. We are a growing and dynamic MNC having head office in Kolkata, India with branch offices in Bengaluru, Kolkata and international offices in Chicago (USA) and Toronto (Canada). We are serving and delivering IT solutions to customers in India and worldwide. Experience: 8+ Yrs Location: Bangalore Job Description: Good experience in Stress Analysis experience in Aerospace Domain. Should have good experience in Aerostructure Analysis Able to analyse stress (Static and Fatigue) and perform hand calculation Experience with FEM tool (Hyperworks /Nastran /Patran) Good technical leadership and delivery management skill Preferred Experience : Experience in DTA (Damage Tolerance Analysis)

Minimum 5-15 years experience in aerostructure analysis, with minimum of 5 years of experience in composite analysis. Thorough familiarity with primary and secondary aircraft structures and load behaviours An Analysis Engineer is required to support stress analysis of aerostructures. The candidate is required to be capable, flexible, and to be able to work independently to assess both composite and metallic design solutions using a variety classical stress methods and finite element analysis. • Be able to conduct a variety of stress analysis on both composite and metallic structures including general strength analysis, stiffness assessments, buckling and stability strength, fastener and joint strength, standard composite strength analysis of both sandwich and thermoset composite panels, composite damage tolerance analysis of open hole strength and compression-after-impact strength. • Have a good understanding of structural design (e.g. Wingbox) including understanding load and stiffness requirements, design of load interfaces such as flap and moveable surfaces and wingbox to fuselage connections • Be able to perform finite element analysis using GKN recognized toolsets (such as Nastran/Patran, Simcenter 3D). Candidate should be capable of creating, modifying, and post-processing results from FEM models. • Generate stress documentation including reserve factor summaries, detailed stress justifications, and certification reports • Perform all activities at a level of minimal supervision and guide other engineers within the work package as required. • Identify, analyse and resolve technical problems and apply/integrate solutions. • Develop, execute, and verify methods plans, toolsets and approaches that are appropriate and compliant to achieve the design and programme objectives. • Identify and assess technical risk and propose mitigations relevant to the workpackage within assigned programmes/projects. • Be able to interpret and process design data including interfaces, dimensions, materials, parts, manufacturing process requirements, assemblies, and tolerances as part of the stress analysis of components. • Deliver assigned project deliverables, documents, and reports to the required quality standards and within the assign project target milestones. • Work within a team environment both locally and remotely. • Support and participate in technical and customer reviews, including formal gate reviews, including the creation and preparation of technical data and presentations of a work package. • Support the qualification process of products within a work package, and prepare and/or check compliance Roles and Responsibilities Execute engineering duties such as Stress Analysis of Mechanical components of Aero Structure, using Simcenter3D, Hypersizer/HyperX, MSC Nastran/Patran. Knowledge of composite stress is mandatory. Experience on eVTOL and AAM is an advantage

The ideal candidate should possess a good understanding of engineering basics and a thorough knowledge of the product life cycle and downstream activities. Strong expertise in Ansys, Nastran, Patran procedures, and methods is essential, along with experience in wings, fuselage, and high lift structures. Proficiency in drawing reading and G&DT is required. The candidate must hold a Bachelor of Engineering degree in Mechanical Engineering and have a basic knowledge of fatigue, finite element analysis, and manufacturing processes. Good knowledge of aero engine components, stack-up layout and calculations, manufacturing processes including heat treatment and welding, as well as hand calculations, is necessary. Familiarity with GD&T, assembly techniques, and assembly processes is essential. Preferred qualifications include experience in ISAMI Ansys, Nastran, Patran, and aero structure component analysis.,

As an Aerospace Structural Stress Engineer with 3-11 years of experience, your role will involve contributing to the Sizing and Justification phase for Aircraft structures. You should have desirable experience working with ATA chapters such as Fire Protection, Flight controls, Fuel, Hydro-mechanical, Landing Gear, Pneumatic, Ice and Rain Protection. In this position, you will be required to apply procedures, manuals, and tools provided by the customer. Your responsibilities will include conducting static and fatigue analysis using both Classical and Finite Element (FE) based approaches. Proficiency in tools such as Hyperworks, Patran, Nastran, CATIA, and Excel Macro (Basic) is essential. You should also have experience in FE modeling for metallic and composite parts, including Fastener modeling. We are looking for a candidate who demonstrates excellent fundamentals in structural engineering, along with strong analytical and problem-solving skills. Your ability to collaborate effectively across functional teams and organizations will be crucial in this role. Strong verbal and written communication skills in English are also required. If you meet these qualifications and are looking for a challenging opportunity in Bangalore with an immediate to 15 days notice period, we encourage you to apply with your Bachelor's degree in mechanical, aerospace, Applied Mechanics, or Structural engineering.,

As a Senior Aerospace Stress Engineer, you will be responsible for performing detailed static analysis on aerostructures, including wings, fuselage, landing gear, floor beams, doors, and other aircraft components using classical hand calculations. Additionally, you will utilize Finite Element Analysis (FEA) software such as HYPERMESH, NASTRAN, and PATRAN to model and analyze structural performance under various loading conditions. Your role will involve ensuring compliance with aerospace industry standards, including FAA, EASA, and military regulations, and actively participating in design reviews. Experience with Airbus and Boeing aircraft structures is considered an added advantage. You will be tasked with developing and validating analytical methods using Excel and Macros techniques to predict the behavior of structural components. Working closely with design engineers, you will provide input on material selection, design changes, and manufacturing processes to optimize structural performance, minimize weight, and maintain safety standards. Furthermore, you will lead the preparation of technical reports and documentation to communicate analysis results, design recommendations, and compliance to regulatory bodies and customers. This includes preparing certification standard reports with detailed explanations of procedures followed for analyzing a structure to support Preliminary Design Review (PDR) and Critical Design Review (CDR). Mitigations and summarizing Reserve factor should be included in the report. As a mentor, you will provide guidance to junior engineers and analysts. Collaboration with cross-functional teams, such as materials, design, and systems, will be essential to ensure integrated, efficient, and safe structural designs. Your responsibilities will also include identifying and addressing structural performance risks, providing solutions to enhance overall reliability and performance of aerostructures. You will participate in customer-facing discussions and presentations related to structural design and analysis. Conducting optimization studies to enhance structural efficiency, reduce weight, and improve manufacturability of fuselage components will be part of your role. Exploring design alternatives to achieve optimal performance is also a key aspect of your responsibilities. To qualify for this position, you should have a Bachelor's or Master's degree in Aerospace Engineering, Mechanical Engineering, or a related field, along with 10+ years of experience in stress analysis and design of aerostructures, preferably in the aerospace industry. In-depth knowledge of structural analysis methods, including finite element modeling (FEM), classical hand calculations, and failure theories is required. Proficiency in FEA tools such as NASTRAN, PATRAN, or HYPERMESH is essential. You should possess a strong understanding of aerospace materials, including composites, metals, and advanced alloys, as well as familiarity with aircraft systems and the integration of structures with other aircraft systems. Knowledge of aerospace loads and regulatory standards and certifications (e.g., FAA, EASA) is also necessary. Strong problem-solving skills, attention to detail, and the ability to manage multiple projects simultaneously are important for success in this role. Excellent written and verbal communication skills, including technical report writing and presentations, will be crucial. Additionally, the ability to thrive in a fast-paced, multidisciplinary team environment is essential for this position.,

Project Role : Manufacturing Engineering Practitioner Project Role Description : Define processes to fabricate, assemble, inspect and test new products and machines based on production engineering and design principles. Define the supporting tools and fixtures needed for production. Develop procedures, product specifications and define the quality standards and inspection methods. Must have skills : Aircraft Structural Analysis Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications. The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as team lead (45 members) for structural analysis and stress evaluationsTechnical customer liaison; deliver training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisExpertise in specific tools/methodologies for the OEMStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:5-8 years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru 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 : NAMinimum 2 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications.The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as key team member for structural analysis and stress evaluationsIndependent technical; deliveries, training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisExpertise in specific tools/methodologiesStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:2-5 years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru 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 : NAMinimum 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications. The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. The ideal candidate will possess, Excellent problem-solving skills, Strong attention to detail and strong ability to manage multiple projects simultaneously Roles & Responsibilities:Serve as SME and team lead (1015 members) for structural analysis and stress evaluationsTechnical customer liaison; deliver training and guide teamPerform analysis using HyperWorks, ISAMI, Nastran/PatranPrepare and review stress certification dossiersCreate, validate, and integrate GFEM/DFEM modelsA350/A350F experience with OEM tools/methods preferred Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs, with strong expertise in OEM-specific tools and methodologies.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Crippling Junctions and Joints) as well as classical hand calculations.Skilled in leading and managing teams of 1015 engineers, ensuring project milestones and quality standards are met.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements.Proficient in metallic/composite structure stress analysisStrong manual/automated stress calculation and airworthiness complianceEffective communication, mentoring, and leadershipProgramming (VBA/Python) and CATIA knowledge is advantageous Additional Information:8+ years' aerostructure stress analysis experience15 years full-time educationBased in Bengaluru Qualification 15 years full time education

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

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

Project Role : Manufacturing Engineering Practitioner Project Role Description : Define processes to fabricate, assemble, inspect and test new products and machines based on production engineering and design principles. Define the supporting tools and fixtures needed for production. Develop procedures, product specifications and define the quality standards and inspection methods. Must have skills : Fatigue & Damage Tolerance F&DT Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :As a Manufacturing Engineering Practitioner, you will define processes to fabricate, assemble, inspect, and test new products and machines based on production engineering and design principles. You will also define supporting tools and fixtures needed for production, develop procedures, product specifications, and define quality standards and inspection methods. Roles & Responsibilities:- Expected to perform independently and become an SME.- Required active participation/contribution in team discussions.- Contribute in providing solutions to work-related problems.- Develop innovative manufacturing processes to improve efficiency.- Collaborate with cross-functional teams to optimize production workflows. Professional & Technical Skills: - Must To Have Skills: Proficiency in Fatigue & Damage Tolerance F&DT.- Strong understanding of structural analysis and material properties.- Experience in CAD software for designing manufacturing processes.- Knowledge of industry standards and regulations for product quality assurance. Additional Information:- The candidate should have a minimum of 3 years of experience in Fatigue & Damage Tolerance F&DT.- This position is based at our Bengaluru office.- A 15 years full-time education is required. Qualification 15 years full time education

Dear Candidate: Greetings from Metrics Numero Talent Acquisition Team!!! MetricsNumero was founded with the goal of creating a centre of excellence that provides high-quality services in Aerospace , Mechanical, SAP, Microsoft, AI/ML, EDW-BI & Data Analytics, Cloud services Mechanical Engineering & Design, ERP and Banking solutions to a wide range of industries globally. Our driving force is to provide innovative solutions to complex business problems. We are specialized in Software Advisory & Consultation. We are a growing and dynamic MNC having head office in Kolkata, India with branch offices in Bengaluru, Kolkata and international offices in Chicago (USA) and Toronto (Canada). We are serving and delivering IT solutions to customers in India and worldwide. Experience: 8+ Yrs Location: Bangalore Job Description: Good experience in Stress Analysis experience in Aerospace Domain. Should have good experience in Aerostructure Analysis Able to analyse stress (Static and Fatigue) and perform hand calculation Experience with FEM tool (Hyperworks /Nastran /Patran) Good technical leadership and delivery management skill Preferred Experience : Experience in DTA (Damage Tolerance Analysis)

Role & responsibilities This position is responsible for supporting Lead Engineers and/or senior level Engineers in the structural substantiation of the mechanical / payloads / systems and structures design within the Technical Services Engineering departments utilizing established modeling and analysis standards (such as Bruhn, Niu, BDM, JA Stress Manuals, etc.). The Stress Engineer will support design and structural substantiation of aircraft engineering packages based on customer and OEM requirements for production, retrofit applications and product development. Work independently and/or under the direction of an experienced engineer, review/analyze basic mechanical/structural/payloads/systems based on defined requirements using approved processes and tools, with knowledge and hands-on experiences in Aircraft monument: FEM, interface load report, substantiation plan, stress analysis, partial static test plan and report, full scale static test plan and report, wind milling analysis Aircraft seating system: FEM, stress analysis, interface load report, dynamic test plan and report, static test plan and report, dynamic simulations Airframe: airframe (fuselage) stress analysis, aircraft fatigue and damage tolerances, Materials: Allowable test plan and report, metallic and composite material properties, material and process specification Regulation and Certification: FAR, CS, SAE, TSO, ACs +Assigned tasks include but not limited to: assemblies/components structural review/analysis, mechanical/structural/payloads/ systems installations review/analysis, specifications review (such as materials specifications and manufacturing process specifications), basic test plans/reports (such as tie-rods tension/compression testing) and associated testing support as needed. Participates in teams to support the development of designs. Supports the documentation of design implementation. Perform engineering design reviews and sign drawings and/or documents. Obtain, interpret, and analyze OEM airplane install drawings using approved processes and tools. Provides technical, design and informational support for airplane modifications (including full-time on-site modification support and on-call home-team support), manufacturing support and/or in-service issues. Troubleshoots basic mechanical/structural/payloads/systems problems associated with structural requirements. Actively support engineering department goals and initiatives. Coordinate with other departments as necessary. Utilize internal analysis/drawing/document standards per customer or regulatory agency requirements. Fast produce error-free engineering documents per engineering document standard. Preferred candidate profile Education and/or Experience Degree in Mechanical Engineering, Aerospace Engineering or related Engineering field and 3-8 years of relevant working experience. Knowledge and Skills: Design: Able to read and understand Computer Aided Design (CAD) designs, drawings and specifications. Knowledge of design techniques, tools and principles involved in production of precision technical plans, drawings, and models. Tools: Proficient in CAE/CAD modeling tools used by the department (such as Catia, AutoCAD, Patran/Nastran, Femap/Nastran). Administration: Knowledge of business and management principles involved in strategic planning, equipment allocation/management, basic leadership techniques and coordination of people and resources. Able to work in a team environment and accept required roles, responsibilities and accountability. Aircraft Fundamental Knowledge: basic knowledge of FAA requirements for the installation and structural substantiation of mechanical/structural/payloads/systems components (14 CFR Part 25, MMPDS, etc.) and OEM Design requirements (Boeing Design Manual, Standard Interface Documents, etc.) is required. Basic understanding of aircraft terms, design and structural analysis requirements is desirable. Engineering: Knowledge of the practical application of engineering science and technology. This includes applying principles, techniques, procedures, and equipment to the design review and structural analysis of various systems, goods and services. Skills Problem Solving: Identifying complex problems and reviewing related information to develop and evaluate options and implement solutions. Critical Thinking: Using logic and reasoning to identify the strengths and weaknesses of alternative solutions, conclusions or approaches to problems. Using scientific rules and methods to solve problems is required. Mathematical: College level mathematics required. Ability to use various formulas embedded and linkage amongst cells in spreadsheet program. Basic statistics required to be able to examine/reduce data and identify results/trends. Finite Elements Method (FEM) mathematics understanding. Customer Orientation: Must demonstrate concern and take actions to meet requirements and high standards of quality of both internal and external customers. Must display courtesy and sensitivity. Manage difficult situations. Meet commitments. Respond promptly to customer needs. Solicit customer feedback to improve service. Communication: Giving full attention to what other people are saying, taking time to understand the points being made, asking questions as appropriate and not interrupting at inappropriate times. Communicating effectively in writing as appropriate for the needs of the audience. Talking to others to convey information effectively. Good oral and written communication skills. Language: Ability to read, analyze, and interpret general business periodicals, procedures, drawings, technical data, engineering documentations, and governmental regulations. Ability to write engineering documentations and formal business correspondence. For situations concerning Japanese customer assignments, Japanese language skills may also be required. Judgment and Decision Making: Considering the relative costs and benefits of potential actions to choose the most appropriate one. Time Management : Managing one's own time. Able to multitask and work independently. Attitude: Demonstrate continuous skill improvement. Positive attitude is required. Other General Requirements: High attention to detail. Able to work in a team environment and accept required roles, responsibilities, and accountability. Able to multitask and work independently. Working knowledge of Windows based computers, particularly MS Office products (Word, Excel Access & PowerPoint). Demonstrate continuous skill improvement. Language Skill: Ability to read and interpret documents such a safety rules, operating and maintenance instructions and procedure manuals. Ability to write routine reports and correspondence. Ability to speak effectively before groups of customers of employees of organization. Reasoning Ability: Ability to apply common sense understanding to carry out instructions furnished in written, oral, or diagram form. Ability to deal with problems involving several concrete variables in standardized situations. Customer Orientation: Must demonstrate concern and take actions to meet requirements and high standards of quality of both internal and external customers. Must display courtesy and sensitivity. Manage difficult situations. Meet commitments. Respond promptly to customer needs. Solicit customer feedback to improve service.

About The Role Project Role : Manufacturing Engineering Practitioner Project Role Description : Define processes to fabricate, assemble, inspect and test new products and machines based on production engineering and design principles. Define the supporting tools and fixtures needed for production. Develop procedures, product specifications and define the quality standards and inspection methods. Must have skills : Aircraft Structural Analysis Good to have skills : NAMinimum 3 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications.The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. Roles & Responsibilities:-Expected to be an SME, collaborate and manage the team to perform.-Capable of handling the customer technically.-Technical Training and guiding the team.-Handling the team of min 10 to 15 members.-Highly preferred A350/A350F primary and secondary structure experience with good knowledge of Excellent problem-solving skillsStrong attention to detailThe ability to manage multiple projects simultaneously-Good Experience in Hyperworks, ISAMI and Nastran/Patran-Experience in GFEM/DFEM creation, validation, and condensation-Preparation/Checking of Stress Certification Dossiers.-Having VBA/Python programming, Catia is an added advantage. Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs, with strong expertise in Airbus-specific tools and methodologies.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Junctions and Joints) as well as classical hand calculations.Skilled in leading and managing teams of 1015 engineers, ensuring project milestones and quality standards are met.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements. Additional Information:- The candidate should have a minimum of 8 years of experience in Aerostructure stress analysis.- This position is based at our Bengaluru office.- A 15 years full time education 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 5 year(s) of experience is required Educational Qualification : 15 years full time education Summary :We are seeking an experienced Aircraft Structures Engineer to join our dynamic aerospace engineering team. The successful candidate will be responsible for the analysis, evaluation, and optimization of aircraft structural components, ensuring compliance with industry standards, safety regulations, and performance specifications.The role involves utilizing advanced engineering software and analytical methods to conduct structural analysis and stress evaluations. A strong background in aerospace structural engineering is essential, including extensive knowledge of materials, structural mechanics, and finite element analysis (FEA) tools. Roles & Responsibilities:-Expected to be an SME, collaborate and manage the team to perform.-Capable of handling the customer technically.-Technical Training and guiding the team.-Handling the team of min 10 to 15 members.-Highly preferred A350/A350F primary and secondary structure experience with good knowledge of Excellent problem-solving skillsStrong attention to detailThe ability to manage multiple projects simultaneously-Good Experience in Hyperworks, ISAMI and Nastran/Patran-Experience in GFEM/DFEM creation, validation, and condensation-Preparation/Checking of Stress Certification Dossiers.-Having VBA/Python programming, Catia is an added advantage. Professional & Technical Skills: Proficient in primary and secondary structural analysis for A320SA, A350, and A350F programs, with strong expertise in Airbus-specific tools and methodologies.Experienced in stress analysis of metallic and composite aircraft structures using ISAMI (CFH, MFH, CFA/MFA, MSP, CSPS, DT TI, DT EI, Unfolding, Junctions and Joints) as well as classical hand calculations.Skilled in leading and managing teams of 1015 engineers, ensuring project milestones and quality standards are met.Extensive hands-on experience with HyperWorks, ISAMI, and Nastran/Patran for structural analysis and simulation.Proficient in the creation, validation, and condensation of GFEM/DFEM models.Adept at technical communication and coordination with customers, ensuring alignment with engineering requirements.Experienced in mentoring and technically guiding team members, including delivering training sessions.Competent in the preparation and peer-review of stress certification dossiers in compliance with regulatory and customer requirements.Additional skills include programming with VBA/Python and proficiency in CATIA, enhancing automation and CAD integration capabilities.Strong ability to perform and accurately interpret both automated and manual stress calculations.Demonstrated understanding of static compliance with customer and airworthiness authority requirements. Additional Information:- The candidate should have a minimum of 8 years of experience in Aerostructure stress analysis.- This position is based at our Bengaluru office.- A 15 years full time education is required. Qualification 15 years full time education

Perform detailed static analysis using classical Hand calcualtion, on aerostructures, including wings, fuselage, landing gear, Floor beam, Doors and other aircraft components. Utilize Finite Element Analysis (FEA) software, such as HYPERMESH, NASTRAN, PATRAN to model and analyze structural performance under various loading conditions. Ensure compliance with aerospace industry standards, including FAA, EASA, and military regulations, and participate in design reviews. Experience on Airbus and Boeing Aircraft structures is an added advantage. Develop and validate analytical methods using excel and Macros techniques to predict the behavior of structural components. Work closely with design engineers to provide input on material selection, design changes, and manufacturing processes to optimize structural performance and minimize weight while maintaining safety. Lead technical reports and documentation to communicate analysis results, design recommendations, and compliance to regulatory bodies and customers. Preparing the certification standard report with detailed explanations of procedures followed for analyzing a structure to support PDR and CDR. Include all the mitigations and summarize Reserve factor in the report Mentor and provide guidance to junior engineers and analysts. Collaborate with cross-functional teams (materials, design, systems, etc.) to ensure integrated, efficient, and safe structural designs. Identify and address structural performance risks, and provide solutions to improve the overall reliability and performance of aerostructures. Participate in customer-facing discussions and presentations related to structural design and analysis. Conduct optimization studies to enhance structural efficiency, reduce weight, and improve manufacturability of fuselage components. Explore design alternatives to achieve optimal performance Bachelor's, Master's, in Aerospace Engineering, Mechanical Engineering, or a related field. 10+ years of experience in stress analysis and design of aerostructures, preferably in the aerospace industry. In-depth knowledge of structural analysis methods, including finite element modeling (FEM), classical hand calculations, and failure theories. Proficient in FEA tools such as NASTRAN/PATRAN/HM similar software. Strong understanding of aerospace materials, including composites, metals, and advanced alloys. Familiarity with aircraft systems and the integration of structures with other aircraft systems. Solid understanding of aerospace loads and regulatory standards and certifications (e.g., FAA, EASA). Strong problem-solving skills, attention to detail, and ability to manage multiple projects simultaneously. Excellent written and verbal communication skills, including technical report writing and presentations. Ability to work in a fast-paced, multidisciplinary team environment.

Key Responsibilities: Perform high-quality mesh generation for structural analysis using Hypermesh and Patran . Develop and refine GFEM and DFEM models for various components and assemblies, ensuring mesh quality and compliance with CAE standards. Prepare models for static, dynamic, and thermal FEA simulations. Interpret and apply engineering drawings and CAD data to build accurate finite element models. Ensure mesh quality and convergence to meet analysis requirements. Ensure adherence to customer-specific FEM guidelines and industry best practices. Collaborate closely with design, simulation, and test teams to validate and iterate FE models. Document meshing processes, model assumptions, and preprocessing methodologies. Troubleshoot and resolve issues related to meshing and model setup. Familiarity with optimization techniques for FE modeling. Required Skills & Qualifications: Bachelor's or Master's degree in Mechanical, Aerospace, or related engineering field. 3 to 7 years of relevant CAE experience , with a focus on meshing and preprocessing. Strong command of Hypermesh and Patran for shell and solid meshing. Hands-on experience in GFEM and DFEM meshing techniques and standards. Solid understanding of FEA fundamentals, material properties, and boundary conditions. Familiarity with CAD software (e.g., CATIA, NX) for model extraction and cleanup. Excellent problem-solving and communication skills. Ability to manage multiple tasks and meet tight deadlines. Proactive attitude towards continuous improvement and learning. Preferred: Exposure to solver environments like OPTISTRUCT , NASTRAN , ABAQUS for FE model set-up Experience with scripting or automation (e.g., TCL, Python) in preprocessing. Knowledge of aerospace or automotive domain-specific CAE workflows.