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Evaluation of the real life vibration regime and its laboratory equivalent for a helicopter carried structure. Part II: derivation of the testing conditions

机译:对直升机携带结构的真实振动制度的评估及其实验室等效。第二部分:测试条件的推导

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摘要

Part II of the paper presents results of the implementation of the generation methods for the simulation program, methods of evaluating the vibration transmission paths and their significance to the simulation program development.
机译:本文的第II部分提出了实施模拟程序的生成方法的结果,评估振动传输路径的方法及其对模拟程序开发的重要性。

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