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Test methods and equipment-model KC-135 airplane wing fatigue test

Application and control of continuously varying loading which simulate flight loading, producing the fatigue damage encountered by aircraft structure can be accomplished electro-hydraulically with results comparable to actual airplane service experience

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  1. The Boeing Company, Transport Division, Technology Laboratory, Renton, Wash.

    Clarence E. Kutz Jr. (Research Engineer)

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  1. Clarence E. Kutz Jr.
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Kutz, C.E. Test methods and equipment-model KC-135 airplane wing fatigue test. Experimental Mechanics 3, 168–172 (1963). https://doi.org/10.1007/BF02327425

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  • DOI: https://doi.org/10.1007/BF02327425

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