Unified system of procedures is developed for estimating some important classes of in-flight noise environments and resulting surface vibration on typical launch vehicle; noise environments are classified according to nature of spatial and temporal correlations of associated fluctuating pressure fields; structural elements considered are cylinder and flat plate; some numerical examples are presented for estimates of frequency spectra of acceleration on vibrating structures; applicable also to orthotropic and liquid-loaded structures.
Response of structural components of launch vehicle to in-flight acoustic and aerodynamic environments
U S Naval Research Laboratory -- Shock and Vibration Bul
United States. Office of Naval Research -- Shock, Vibration and Associated Environments -- Bulletin ; Bul 36, Part 5 ; p 97-106
1967
10 pages
Report
Englisch
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