Engineer III - Structures

Location: Bangalore, India

Department: N-CCAV

Experience: 3-4

• 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.

• 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.
• Good Knowledge of Composite Materials and Sizing criteria of Composite parts

• Experience in structural design of unmanned aerial vehicles.