150 Static Analysis Jobs

The development/Tools & Infrastructure team ofthe 'Enterprise Manager' is looking for a motivated 'Tools/Infrastructure Developer' with 3+ years of experience, skilled good scripting experience in Python, Perl, Javascript & Shell on Linux platform, along with expertise in code coverage infrastructure and static code analysis tools who would like to help with the advanced state-of-the-art technology for building, configuring, and deploying cloud software. Requirements: Proficiency in scripting languages (ie. Python, Perl, Javascript, Shell) Extensive working knowledge of Unix/Linux, Windows(optional) Experience with Static code analysis tools like SonarQube, Fortify Experience with code coverage infrastructure like Jacoco Experience with the build management tools like Gradle/Maven, Make Strong understanding and knowledge of SDLC/Agile Methodologies & CI/CD Processes. Solid analytical and problem-solving ability along with excellent English communication skills & ability to quickly learn new technologies. Good to Have: Prior experience with Automation framework, Tools & Infrastructure development Experience in Database like 'Oracle' & SQL Programming Familiarity with popular DevOps technologies such as Git/Bitbucket, Jenkins/TeamCity, Artifactory, and Jira/Confluence. Docker/Podman Education: B.E/B.tech (or M.E/M.Tech) in Computer Science / Information Technology or equivalent. Career Level - IC3 Responsibilities The team leverages best-of-breed open source technology to automate the infrastructure used to build and deploy the product. Areas the team is working on include product build, integration, provisioning, deployment performance optimization, and integrating new technology to improve the developer experience. As a member of the software engineering division, you will assist in defining and developing software for tasks associated with the developing, debugging or designing of software applications or operating systems. Provide technical leadership to other software developers. Specify, design and implement modest changes to existing software architecture to meet changing needs. Qualifications

We are looking for a highly skilled and motivated Product & Solution Security Professional to join our team. We are looking for proven experience of 15 years in cybersecurity, with a focus on application security and proven experience working with software development teams and integrating security practices into the SDLC. Experience interacting with key collaborators and supporting security activities within software products. Having An engineering degree B.E/B.Tech/MCA/M.Tech/M.Sc with good academic record. The ideal candidate will be responsible for defining secure design principles and supporting multi-functional teams to ensure secure architecture, implementation, and testing of products and solutions. Integration with SDLC: Collaborate with software development teams to integrate security practices throughout the Software Development Life Cycle (SDLC). Ensure security requirements are included in the design, development, testing, and deployment stages of software projects. Perform security code reviews and analyze vulnerabilities during different SDLC phases. 2. Security Activities: Develop and implement security protocols, guidelines, and standard processes for software development. Conduct threat modelling and risk assessments to identify potential security issues early in the development process. Provide guidance on secure coding practices and remediation of identified vulnerabilities. 3. Stakeholder Interaction: Work closely with key collaborators, including product managers, project managers, and business analysts, to support and promote security activities within products. Communicate security risks, issues, and mitigation strategies effectively to both technical and non-technical collaborators. Foster a security-aware culture within the development teams and across the organization. 4. Security Tools and Technologies: Implement and manage security tools such as static and dynamic analysis tools and vulnerability scanners. Stay updated with the latest security tools, trends, and standard methodologies to enhance products security posture. 5. Training and Awareness: Conduct security training and awareness programs for development teams. Promote continuous improvement related to application security. Skills and Qualifications: Technical Skills: In-depth knowledge of application security, secure coding practices, and common vulnerabilities (e.g., OWASP Top Ten). Experience with security tools and technologies such as static analysis tools (SAST), dynamic analysis tools (DAST), and vulnerability scanners. Proficiency in programming languages such as Java, C#, Python. Understanding of DevSecOps practices and integration of security into CI/CD pipelines. Promote continuous improvement and related to application security. 2. Soft Skills: Strong communication and interpersonal skills. Ability to explain complex security concepts to non-technical collaborators. Strong analytical and problem-solving skills. Collaborative approach and ability to work effectively with multi-functional teams. 3. Certification Preferred: CEH, Certified Secure Software Lifecycle Professional (CSSLP) or equivalent

Core AI is at the forefront of Microsoft's mission to redefine how software is built and experienced. We are responsible for building the foundational platforms, services, programming models, and developer experiences that power the next generation of applications using Generative AI. Our work enables developers and enterprises to harness the full potential of AI to create intelligent, adaptive, and transformative software. The Future of Scalable Software Engineering ( FoSSE ) team's objective is to build capabilities to enable AI-enabled modernization of very large code bases on a large scale and with very high quality. Job Purpose Overview In this role, you will help define the future of software development. Y ou will help build and combine static analysis and ML tools to help AI handle the scale of large code bases. You will work with state-of-the-art LLMs and reasoning models, very large code bases, and use data from pull requests, static analysis warnings reports, and developer feedback from AI recommendations to build AI agents that scale. You will grow by developing both static analysis and ML based techniques that are needed to build coding agents that scale to large code bases. You will be onsite 3 days a week and learn and grow through working with talented colleagues. Standard Company, Culture, Candidate Value Proposition - Use the following: Microsoft's mission is to empower every person and every organization on the planet to achieve more, and we're dedicated to this mission across every aspect of our company. Our culture is centered on embracing a growth mindset and encouraging teams and leaders to bring their best each day. Join us and help shape the future of the world.

Business Group Overview Core AI is at the forefront of Microsoft's mission to redefine how software is built and experienced. We are responsible for building the foundational platforms, services, programming models, and developer experiences that power the next generation of applications using Generative AI. Our work enables developers and enterprises to harness the full potential of AI to create intelligent, adaptive, and transformative software. The Future of Scalable Software Engineering ( FoSSE ) team's objective is to build capabilities to enable AI-enabled modernization of very large code bases on a large scale and with very high quality. Job Purpose Overview In this role, you will help define the future of software development. Y ou will help build and combine static analysis and ML tools to help AI handle the scale of large code bases. You will work with state-of-the-art LLMs and reasoning models, very large code bases, and use data from pull requests, static analysis warnings reports, and developer feedback from AI recommendations to build AI agents that scale. You will grow by developing both static analysis and ML based techniques that are needed to build coding agents that scale to large code bases. You will be onsite 3 days a week and learn and grow through working with talented colleagues. Standard Company, Culture, Candidate Value Proposition - Use the following: Microsoft's mission is to empower every person and every organization on the planet to achieve more, and we're dedicated to this mission across every aspect of our company. Our culture is centered on embracing a growth mindset and encouraging teams and leaders to bring their best each day. Join us and help shape the future of the world.

MANDATORY SKILLS C++14,GTEST,LINUX,Static Analysis Tool JOB DESCRIPTION v Self-driven person, ability to solve problems by collaborating. v Continuous learning v Good understanding of the Dev and agile process v Able to refine the assigned stories based on previous dev experience v Ability to get and filter the right information from multiple sources (Docs, AI, specifications, requirements) v Understand the importance of quality Analyzing, Implementation and Review skills Must: Able to analyze and identify the gaps in requirement based on tools and existing code Implement the code according to requirement / design and write the unit level test logic to test the implementation Adhere to coding guidelines and quality metrics while implementing code. Identify the coding and quality issue in the code while doing peer review. Identify the missing unit level test implementation while doing peer review Good to have : Propose design changes in the code if required. Understand the limitations of the test infrastructure and ability to create functional test case Able to define test cases based on different scenarios Debug skills Understand the debugging process and effectively debug for corner cases on HW. Possibility to understand and to reproduce if needed a PR received from a customer Collaborate and gather the required information from another team member. Programming skills C++14 : Must 1. STL implementation level understanding (Vector, Array, Map and Unordered Map) 2. Lambda and scope implementation level understanding 3. Smart Pointers implementation level understanding 4. Polymorphism implementation level understanding 5. Understand Mutex, Threading concepts 6. Templates implementation level understanding Tools and Framework: Gtest : Must: 1. Understand the unit testing logic, fixtures 2. Parameterized testing Good to Have: 1. Mocking (gtest) 2. Stub (gtest) Static Analysis Tool: Must Python : Good to have Bazel: Good to have Git Commands: Basics must Adaptive Autosar : Good to have SOME/IP: Good to have Language: Strong written and spoken English skills

Identify & capitalize on new opportunities, expanding the service portfolio & client base. Lead presales activities, crafting compelling proposals & securing new deals. Develop & implement effective sales strategies & GTM plans. Lead the presales process, identifying client needs & presenting customized TVM solutions. Manage key client relationships, ensuring their satisfaction & driving long-term loyalty. Manage relationships with key 3rd parties, ensuring they support practice goals & build new opportunities. Collaborate with internal teams to ensure seamless service delivery & client satisfaction. Contribute to Blogs, Whitepapers, POV. 10-15 years of experience in Application Security Presales. Desirable: Security certifications Extensive knowledge of Red Teaming, DevSecOps, VM, DAST, SAST, IST, IAST, CST, IoTST, & Social Engineering. Strong communication & interpersonal skills. Excellent strategic thinking & business acumen. Passion for client success & service excellence.

We are looking for a Software Toolchain Engineer to join our engineering team. In this role, you will be developing, maintaining, and optimizing software development toolchains, including compilers, linkers, debuggers, build systems, and related infrastructure. In particular, the focus is on Software Development Kit (SDK) porting and retargeting pretrained neural network models on an AI inference engine. You have: Bachelors or Masters degree in Computer Science, Computer Engineering, or related field. 5+ years of experience in software toolchain. Strong proficiency in C/C++, Python, PyTorch. Deep working knowledge of compiler internals and linking/loading processes. Experience in CUDA. Understanding of AI neural-network architectures, and formats such as ONNX. Neural-network optimizations such as model quantization, pruning. Understanding of systems-level topics like memory management, scheduling, and multi-core compute. Experience with version control systems like Git. At least one major compiler infrastructure (e.g., GCC). It would be nice if you also had: Contributions to open-source compiler or toolchain projects. Experience in programming kernel functions. Familiarity with deployment to edge devices or cloud inference platforms. Knowledge of low-level programming, embedded systems, or hardware architectures (CPU/DSP/GPU). Design, develop, and maintain software development toolchain, including compilers, linkers, debuggers, static analysis tools, code generators, and build systems. Adopt and customize third-party and open-source tools and technologies to meet specific needs. Identify bottlenecks and areas for improvement within the existing toolchain. Optimize performance and output for specific hardware targets based on a hardware-accelerated multi-core RISC-V system. Collaborate with AI/ML experts, hardware and embedded software engineers. Develop SDK: native API, libraries, plugin to PyTorch and/or TensorFlow backend. Develop user environment from PyTorch to instruction simulator.

Role Overview: Siemens Energy is dedicated to helping customers address the world's most critical energy challenges. As a global leader in advanced engineering technologies, we aim to enhance lives and advance human achievements while also safeguarding the environment. By joining our team, you can contribute to meaningful work that benefits society and human progress. At Siemens Energy, the focus is on "Energizing society" by assisting customers in transitioning to a more sustainable world through innovative technologies and the ability to bring ideas to life. Key Responsibilities: - Able to conduct various types of FE Analysis such as static, transient, linear, nonlinear, fatigue (LCF/HCF), and thermal analyses as required. - Perform high-temperature creep calculations and assessments. - Interpret analysis results, propose design modifications, and optimize designs. - Participate in and lead structural integrity design reviews at the component level. - Prepare and document FE calculations in the form of structural integrity design reports. Qualifications Required: - Good understanding of mechanical engineering principles. - Proficiency in turbine design and manufacturing. - Strong grasp of FEA principles and methods. - Experience with FEA software like ANSYS, ABAQUS is preferred but not mandatory. - Ability to work both independently and collaboratively within a team. - Excellent problem-solving and analytical skills. Additional Company Details: Siemens is a global organization with a diverse workforce of over 379,000 individuals across more than 200 countries. We are committed to equality and encourage applications that reflect the diversity of the communities we serve. Employment decisions at Siemens are made based on qualifications, merit, and business requirements. Join us with your curiosity and creativity to help shape a better tomorrow.,

Role Overview: As a Code Manager in the Agile Train, your primary focus will be on ensuring code quality, consistency, and integration across the ART (Agile Release Train). You will play a crucial role in managing the codebase and influencing development practices to support the overall release delivery. Key Responsibilities: - Establish and enforce coding standards to maintain consistency in coding practices across all teams within the ART. - Manage code repositories and branching strategies to ensure smooth code management and version control. - Facilitate code reviews and quality checks to maintain a high-quality codebase. - Automate build and integration processes using CI/CD tools like Jenkins, GitLab CI, or Azure DevOps. - Manage code dependencies to ensure proper versioning and compatibility. - Support release engineering activities by handling merging, tagging, and managing release artifacts. - Promote code reuse and maintainability to support rapid and reliable releases. Qualifications Required: - Strong experience with Git or other distributed version control systems. - Expertise in build automation tools such as Jenkins, GitLab CI, or Azure DevOps. - Proficiency in scripting languages like Python or Bash. - Deep understanding of code quality principles and practices. - Experience with static analysis tools and code review tools. - Excellent communication and collaboration skills. - Experience working in an Agile environment. - Familiarity with SAFe or other scaling frameworks is a plus. Additional Details: The role involves a significant emphasis on maintaining code quality, enforcing coding standards, and managing code integration across the Agile Release Train. You will be responsible for ensuring a high-quality, well-integrated codebase that supports predictable and reliable release deliveries. FYR: - Release Manager (Agile Train) is not in scope for this position. - The focus is on overall release delivery for the entire ART, encompassing all teams and components within the ART.,

Responsible for performing structural analysis of aircraft components, assemblies, and systems while working as a coordinated 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 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

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 : 7+ Years Job Location : Bangalore Preferred Skills : Must have relevant Stress Analysis experience in Aerospace Domain. Should have good experience in Aero Structure Analysis Able to analyse stress (Static or Fatigue) and perform hand calculation Experience with FEM (Hyper works /Nastran /Patran)

The C3iHub at IIT Kanpur is in search of a highly motivated and skilled Malware Analysis Researcher to join the cybersecurity research team. As a Malware Analysis Researcher, you will be responsible for conducting static and dynamic analysis of various malware samples, including formats like PE, PDF, ELF, and APK. Automation of analysis tasks using scripting tools such as Python, Bash, or others will be a key aspect of the role. You will also be involved in setting up and maintaining sandbox environments for behavior monitoring and analyzing packed, encrypted, or obfuscated malware through reverse engineering techniques. Additionally, the ideal candidate will have experience in utilizing and contributing to open-source tools like YARA, Volatility, Ghidra, and Radare2. Curating and labeling malware datasets for machine learning pipelines, conducting source code analysis using SAST and DAST tools, and authoring technical documentation are also part of the responsibilities. Furthermore, collaborating with internal teams on threat research, detection model tuning, and proof of concept development will be essential. Occasional travel within India may be required for project-related meetings, demonstrations, or coordination. To be eligible for this position, candidates must hold a Master's degree in Computer Science, Information Security, or a related field, along with at least 2 years of hands-on experience in malware analysis or reverse engineering. Proficiency in scripting languages like Python and Bash, familiarity with threat analysis tools, and a strong understanding of malware behavior, file formats, and analysis techniques are necessary qualifications. Preferred qualifications for the role include specialization in Cybersecurity or Information Security, experience with tools such as IDA Pro, Ghidra, Wireshark, or Sysmon, exposure to ML/AI-based malware classification projects, and research publications in reputable cybersecurity journals or conferences. The successful candidate should be prepared to travel across the country for project execution and monitoring, as well as for coordination with geographically distributed teams. Interested applicants are required to submit a cover letter summarizing their experience in relevant technologies and software, along with a resume and the latest passport-size photograph.,

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

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

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : 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

Job Description Summary Responsible for designing, developing, and testing Embedded Software (Firmware), platforms and systems that control and runs on devices that need to be tailored to the needs of the hardware that it controls and run on. Typically requires a deep understanding of the characteristics of the physical device being controlled, the real-time functions it is expected to perform and the ability to design, develop, implement, and test the logic and software required to realize the real-time functionality. Executes standard operational/technical tasks typically subject to instructions and work routines. As part of a multi-developer firmware team the major responsibilities will include analysis, design, implementation and testing of firmware for Monitoring & Diagnostic devices product line. The Firmware Architect will report to the Engineering Manager Monitoring & Diagnostics team in Hyderabad. Job Description Roles and Responsibilities: Design and modify product architecture and create definition of components and interfaces. Create product integration strategies and modify architecture to meet performance definitions. Design, develop, implement, and debug embedded software and/or firmware features/set of features for a complex module or a large component of entire embedded software product. Integrate software packages with existing systems and sub-systems. Prepare unit test and regression test specification, packages, and templates. Ensure that the development backlog is prioritised and stacked in the optimal order for developers to be as effective as possible Interact with a multi-discipline engineering team to meet the project requirements throughout its life cycle. Prepare formal and informal engineering documentation (e.g., Design documents, code reviews, Release reports etc.). Engages in technical discussions; participates in technical designs and presents technical ideas through white boarding. Works closely with peers and guide in a fast pace technical design and development team, acting as Subject Matter Expert for the developers. Executes in a fast-paced delivery mode and focuses in delivering tasks to meet the product release goal. Maintains code quality through best practices, code reviews and unit testing. Required Qualifications: Bachelors degree in Computer Science, Electrical Engineering, or Electronics Engineering. A minimum of 12 years of embedded development experience. Proficient in Real-Time Embedded Software Engineering in C/C++ on any embeddedprocessor/DSP/Microcontrollerand RTOS (e.g., FreeRTOS, TI-RTOS, VxWorks etc.), File system, Boot, Device drivers. In-depth experience with various firmware architectures. Experience in stack integration and application firmware development. In-depth knowledge of Transmission platform and its applications. Well familiar with HW/SW interfacing, and real-time design consideration. Experience in working with fast network/data interfaces like 1G/10G Ethernet, PCI-E Familiarity with cybersecurity constructs (Static Analysis, Digital Signatures etc.) Familiar with Agile-SW development practices. Desired characteristics: Experience developing multi-threaded/ multi-tasking real time applications. Using emulators, simulators, and software analysis tools and Proficient in debugging code. Sound knowledge of Processors, DSPs (preferably from Analog Devices or TI) and Microcontrollers (preferably ARM cores on Intel or Freescale chips). Cyber security aspects, such as symmetric and asymmetric cryptography and PKI Infrastructure, LDAP, RADIUS, TLS, SSH, SFTP, RSA, HTTPS, is an asset. Excellent working capacity, flexible and ability to cope with periods of high workloads. Robust and solution oriented. Experience in all phases of the product engineering and development cycle. Additional Information Relocation Assistance Provided: Yes

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

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

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : 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.

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

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

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

Project Role : Engineering Services Practitioner Project Role Description : Assist with end-to-end engineering services to develop technical engineering solutions to solve problems and achieve business objectives. Solve engineering problems and achieve business objectives using scientific, socio-economic, technical knowledge and practical experience. Work across structural and stress design, qualification, configuration and technical management. Must have skills : Aircraft Structural Analysis Good to have skills : NA Minimum 5 Year(s) Of Experience Is Required Educational Qualification : 15 years full time education Summary: As a Mechanical Engineering Practitioner, you will design, analyze, and build structures, machines, devices, systems, and mechanical processes. A strategic aerospace engineering leader specializing in rotary wing platforms, with a strong track record in driving technical delivery, innovation, and client satisfaction. Experienced in shaping engineering processes, delivery governance, and team capability development. Proven ability to influence design and compliance strategies through direct engagement with OEMs, Tier-1 suppliers, and regulatory bodies. Passionate about digital transformation, with a focus on advancing MBSE, MBD, and digital continuity across the product lifecycle. Roles & Responsibilities: You will join the Aerostructure Engineering team, contributing across the full engineering lifecyclefrom initial concept and design through certification and build line supportcovering end-to-end (E2E) responsibilities. Key responsibilities include the design and development of primary and secondary structural components (both metallic and composite materials), assemblies, and system installations for a range of fixed-wing and rotary-wing aircraft platforms. Design and develop primary and secondary structural componentsboth metallic and compositefor rotary-wing aircraft, ensuring compliance with airworthiness regulations, structural integrity requirements, and OEM-specific design standards. Understand the meshing and analysis guidelines for static, dynamic and impact analysis and ensure the FE models created by team are complied to the guidelines and are of high quality. Ensure that the V&V documents capture the required checks for the FE models. Also ensure the physics of the problem is correctly simulated in the FE models and if required use your expertise and guidance to align with the requirements. Ensure alignment and compliance to the client specific and regulatory guidelines as per FAR 27/29 /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 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 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