Discussion on experiment in which aerodynamic noise data at high Reynolds numbers obtained in supersonic speed range with aid of launch vehicle were telemetered from vehicle to ground recording station; results indicate shift in spectrum shape as function of Mach number, with higher frequencies corresponding to higher Mach numbers; it was also found that surface-pressure coefficients at supersonic Mach numbers do not vary markedly from those at subsonic Mach numbers for comparable flow conditions; study applicable to supersonic transport and launch vehicles.
Scout-vehicle aerodynamic-noise measurements
Sound
Sound ; 2 , n 5 ; p 28-31
1963
4 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Scout-vehicle aerodynamic-noise measurements.
NTRS | 1963
|NTRS | 1961
NTIS | 1965
|Online Contents | 1994
|NTRS | 1965
|