tattle
发表于 2025-4-1 02:57:26
Evaluation, Modification And Damage Tolerance Of An In-Service Aircraft Critical Areaantitative fractography to develop the test crack growth curves for pre-modification and post-modification. Testing applied the equivalent of seven life times of simulated usage in the two phases of the fatigue testing. This included the required factor of five lifetimes, post-modification, for an u
Adherent
发表于 2025-4-1 06:55:03
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OASIS
发表于 2025-4-1 10:29:20
M. J. BosCoverage of all areas related to aeronautical fatigue and aircraft structural integrity