Experiments made at Purdue Univ Jet Propulsion Center to determine factors which contribute to occurrence of transverse modes of combustion pressure oscillation in rocket motors; results indicated that changes in aspect ratio and volume of rocket motor combustion chamber had profound effect on incidence and amplitude of transverse modes determined to be "spinning" and radial modes.
Importance of combustion chamber geometry in high frequency oscillations in rocket motors
ARS J
ARS Journal ; 31 , n 4
1961
5 pages
Article (Journal)
English
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