A Experimental Study on Combustion-Stability Rating in a Subscale Chamber

모형 연소실에서 분사기 연소 안정성 평가에 관한 실험적 연구

  • Published : 2012.04.13

Abstract

To predict combustion instability in actual full-scale combustion chamber of rocket engines, air-injection test is proposed with scaling techniques. From the data, damping factors have been obtained as a function of hydraulic parameter and the data give us instability map. Two instability regions are presented and it is found that they coincide reasonably with them from hot-fire test with full-scale flow rates. Accordingly, the proposed approach can be applied cost-effectively to stability rating of jet injectors when mixing of fuel and oxidizer jets is the dominant process in instability triggering.

Acknowledgement

Supported by : National Research Foundation of Korea(NRF)