An experimental investigation was conducted to determine the effect of the mixing of gaseous propellants on high-frequency combustion pressure oscillations in a rocket motor. The results indicate the influence of the type of injector, some mixing parameters (injection velocity and momentum flux ratio), the combustion pressure, and the propellant combination. (Author)
Combustion Pressure Oscillations in an Unmixed Gas Rocket Motor
1966
5 pages
Report
Keine Angabe
Englisch
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