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INVESTIGATION AND VALIDATION OF A FLEXURE INTERFACE FOR THE MODAL TESTING OF ORBITER PAYLOADS

机译:轨道有效载荷模态测试的挠性界面的调查与验证

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A reduced scale test of flexural interfaces was conducted to validate the application of the technique to full scale modal testing of orbiter payloads. Flexural interfaces are seen as a hybrid alternative to the traditional fixed or free-free boundary conditions. The data from this effort will be used to design a full scale flexural interface for the testing of Space Station modules.
机译:进行了弯曲界面的减小规模测试,以验证技术在轨道有效载荷的全规模模态测试中的应用。弯曲界面被视为传统固定或无自由边界条件的混合替代品。本努力的数据将用于设计用于空间站模块的测试的全尺度弯曲界面。

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