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About the role
Job Description:
Experience Range: 5-7 Years Only
- Knowledge Fatigue and Damage Tolerance analysis
- Theoretical knowledge in aircraft crack propagation analysis
- Knowledge of aircraft loads and experienced in spectrum generation
- Calculation of Seq stresses (fatigue and crack propagation), understanding of mission profiles, rainflow counting, Miner's rule, stress files, FESPS databases.
- Calculation of Stress concentration (Kt) values using Petersons' or DFEM or ISAMI modules.
- Analysis of metallic and composite structures (Plain Strength checks, Buckling, Bolted joint analysis)
- Knowledge of static and fatigue design values (Ftu, Fty, Fcy, AFI parameters, S-N curve parameters, fracture toughness etc.,)
- Static and Fatigue calculations (Hand calculations, DFEM, ISAMI, GFEM load redistribution)
- Ability to read the drawings and interpret fastener diameter, fastener fit, fastener spec & type, surface protection treatment to be useful for fatigue calculations.
- Possess strong foundation in the area of load/stress analysis with abilities to formulate ""free body diagrams"" and identify load path of structures
- ISAMI modules (Metallic Filled Hole, Composite Filled Hole, Lug analysis, Corin Analysis, Notch Sensitivity, Damage Tolerance, Tension Fitting, Fatigue Spectrum Analysis (1D & 2D), Fatigue DFEM Initiation Modules, etc.,)
- Experienced in documents (like PDR/CDR/Certification reports, Concessions, Repairs) and report creation and getting validated.
This job requires an awareness of any potential compliance risks and a commitment to act with integrity, as the foundation for the Company’s success, reputation and sustainable growth.
Company:
Airbus India Private Limited
Employment Type:
Permanent
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Experience Level:
Professional
Job Family:
Structure & Dynamic Systems Analysis