Improved Vibration Design and Test Procedure for Aircraft
Date Published: 1974-02-01
Paper Number:740815
DOI: 10.4271/740815
Citation:
Beck, C., "Improved Vibration Design and Test Procedure for Aircraft," SAE Technical Paper 740815, 1974, doi:10.4271/740815.
Author(s):
Clark J. Beck - Boeing Aerospace Co.
Abstract:
Recent experience with vibration qualification of avionics for the B-1 airplane has revealed deficiencies in commonly used vibration design and test procedures. Specific examples of deficiencies are discussed. Recommendations for improving vibration design and test procedures are presented in the areas of environment prediction, qualification testing, and use of vibration isolators. Suggestions are made relative to vibration design and testing in light of the “try-before-buy” concept.
File Size: 808K
Product Status: In Stock
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