Titlebook: ICAF 2009, Bridging the Gap between Theory and Operational Practice; Proceedings of the 2 M. J. Bos Conference proceedings 2009 Springer Sc

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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

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OASIS

M. J. BosCoverage of all areas related to aeronautical fatigue and aircraft structural integrity