In the process of developing the variable thrust rocket engine, combustion vibrations are encountered in the low end of the operating conditions. We used a lateral baffle to satisfactorily solve the problem. This paper mainly introduces the experimental results and qualitative analysis. The approach is novel. It can be used as a reference. (Keywords: rocket engines)
Approach of Preventing Combustion Vibrations of Rocket Engine with Lateral Baffle
1987
26 pages
Report
No indication
English
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