Job Description

•Candidate Should have good hand-on work experience in Fatigue and Damage Tolerance Analysis of Airframe Structural Analysis for Airbus Methods •Candidate should have in depth knowledge of Fatigue Design Philosophies •Knowledge and experience in Structural Failure and Fatigue Failure Characteristics •Aware of various types of fatigue, Fatigue assessment Principles and Methods •Calculate Fatigue Analysis of Metallic and Fastener parts using AFI method. •Composite Fatigue Analysis experience •Candidate should have experience in Damage Tolerance Analysis and Crack Propagation using different NASGRO models •Identification of PSE ( Principal Structural Elements ) •Calculate Stress Concentration Factor (Kt). Wide Spread Fatigue Damage Factor, effect in fatigue due to Size, Material, joints, Machining quality, technology process, etc. •Fatigue Index Calculation (AFI) Calculation •Fatigue Equivalent Stress Calculation and extraction of Reference Stresses (1...