This report summarizes the main accomplishments of a three-year research program supported under AFOSR Grant No. F49620-93-1-0177. The main objective of this program was to investigate active suppression of detrimental combustion instabilities in chemical rockets by a controlled, secondary, combustion process. The program consisted of parallel theoretical and experimental efforts; the former developed the theoretical foundation of the investigated control approach and the latter developed a small scale, actively controlled, gas rocket setup that was used to guide the development of the investigated active control system and demonstrate its effectiveness.
Investigation of Active Control of Combustion Instabilities in Chemical Rockets
1996
80 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Combustion & Ignition , Physical & Theoretical Chemistry , Combustion , Instability , Rockets , Optics , Control systems , Pressure transducers , Chemicals , Gases , Combustors , Fuel injectors , Suppression , Chemical rockets , Active control system , Acs(Active control system) , Rayleigh criterion
Investigation of Active Control of Combustion Instabilities in Chemical Rockets
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