SAE-G-5 Aerospace Shock and Vibration Committee was formed to establish stepwise procedure for design of linear, center-of-gravity type vibration isolation systems whose function is to protect fragile equipment, installed on aircraft, missiles or spacecraft, from sinusoidal and random vibrational environments encountered; publication presents philosophy and approach applied, general concepts, concept of vibration source, fragility, outline of theoretical background, and practical application.
Rational procedure for design of vibration isolation systems
SAE -- Paper
1961
28 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Design procedure for vibration isolation on nonrigid supporting structures
Engineering Index Backfile
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Tema Archive | 1974
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