Roles and Responsibilities:

- Create Finite Element models for linear and nonlinear structural analysis, both at component and assembly level.
- Select suitable structural materials to meet strength, weight and other performance/ safety requirements.
- Design experimental test procedures and instrumentation for validation of analytical models.
- Lead aeroelastic and fatigue simulations to evaluate structural stability under dynamic loads.
- Translate analysis/ test results into actionable design recommendations and risk mitigation strategies.
- Plan suitable flight test instrumentation, analysis tools and carry out flight test data analysis for loads and flutter.
- Generate/ review reports for summarising all project-related analysis results.

Must have skills:

- At least 5 years’ experience in design of main aircraft structural components (metallic and composites), especially from aeroelastic and fatigue considerations.




- Experience in static and dynamic analysis (Modal, transient, random vibration) of aircraft structures.
- Experience in selection of suitable structural materials and design and manufacturing of composite parts.
- Possess advanced FEA skills
- Knowledge of aeroelasticity related modelling and simulation.
- Knowledge of CAD software e.g., CATIA, SolidWorks.
- Awareness of airworthiness certification requirements based on analysis and testing.
- Organizational and time management skills.
- Ability to work solitary or in a team.
- Positive Knowledge of Composite Materials and Sizing criteria of Composite parts

Good to have skills:

- Experience in structural design of unmanned aerial vehicles.

📌 Engineer III - Structures (India)
🏢 Newspace
📍 India