Description
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 a…
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