Titlebook: Shock & Vibration, Aircraft/Aerospace, Energy Harvesting, Acoustics & Optics, Volume 9; Proceedings of the 3 Anders Brandt,Raj Singhal Conf

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2191-5644 ting Data Applications.• Aerospace Testing Techniques.• Aircraft /Aerospace Applications.• Joints.• Acoustics & Optics.• Other Sensing.978-3-319-80721-8978-3-319-30087-0Series ISSN 2191-5644 Series E-ISSN 2191-5652

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A Study on the Dynamic Interaction of Shock Response Fixtures and Test Payload,, customization of the shock response input is necessary..This work focuses on the identification as to how the article under test is affected by the attachment to the excitation fixture. Models are presented to show how the test article response is distorted by the dynamic interaction with the test fixture.

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Force Limited Vibration Using the Apparent Mass Method,mption that the test article and its in-service mounting structure are lightly damped, and that the in-service forces exciting the mounting structure are broadband. The resulting equation is shown by numerical example to produce significant notching without producing an under-test situation, even for extremely light test articles.

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