Structural fatigue induced by random vibration often sizes bracket structures in modern aerospace vehicles; this study reports results of experimental study conducted to evaluate design factor approach for application to fatigue problem which would account both for dynamic characteristics of system and fatigue characteristics of materials; study established feasibility of utilizing equivalent static design factors in basic bracket design by postulating required factors and then obtaining these factors through fatigue tests on simple cantilever beams.
Evaluation of design factor approach to space vehicle design for random vibration environments
U S Naval Research Laboratory -- Shock Vibration Bul
U S Naval Research Laboratory -- Shock and Vibration Bulletin ; Bul 35, Part 5
1966
36 pages
Aufsatz (Zeitschrift)
Englisch
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