The role requires a professional with 5-7 years of experience specifically in fatigue and damage tolerance analysis for aircraft structures
Job Summary
The role requires a professional with 5-7 years of experience specifically in fatigue and damage tolerance analysis for aircraft structures.
Candidates must possess deep theoretical knowledge of crack propagation, spectrum generation, and the ability to calculate stress concentrations using specialized modules like ISAMI and DFEM.
The position involves analyzing both metallic and composite structures while ensuring compliance with static and fatigue design standards including S-N curves and fracture toughness.
Matching Summary
The role requires a professional with 5-7 years of experience specifically in fatigue and damage tolerance analysis for aircraft structures.
Skills & Requirements
Must-have
5-7 years experience in fatigue analysis
Knowledge of aircraft crack propagation
Spectrum generation and rainflow counting
Miner's rule application
Stress concentration calculation using Petersons or DFEM
ISAMI modules proficiency
Static and fatigue design values expertise
Nice-to-have
Strong foundation in load path identification
Experience with certification reports and concessions
Ability to read complex engineering drawings
Commitment to compliance risks and integrity
Flexible working arrangements awareness
Key Requirements
5-7 years of relevant experience
Proficiency in ISAMI and DFEM modules
Understanding of mission profiles and fastener specifications