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A Numerical Study on Combustion-Stability Rating of Impinging-Jet Injector Using Air-Injection Technique

공기분사 기법을 이용한 충돌형 제트 분사기의 연소 안정성 평가에 관한 수치적 연구

  • 손채훈 (조선대학교 항공우주공학과) ;
  • 박이선 (조선대학교 대학원 항공우주공학과)
  • Published : 2006.11.01

Abstract

Combustion stability rating of jet injector is conducted numerically using air-injection technique in a model chamber, where air is supplied to oxidizer and fuel manifolds of the model five-element injector head. A sample F(fuel)-O(oxidizer)-O-F impinging-jet injector is adopted. In this technique, we can simulate mixing process of streams flowing through oxidizer and fuel orifices under cold-flow condition without chemical reaction. The model chamber was designed based on the methodologies proposed in the previous work regarding geometrical dimensions and operating conditions. From numerical data, unstable regions can be identified and they are compared with those from air-injection acoustic and hot-fire tests. The present stability boundaries are in a good agreement with experimental results. The proposed numerical method 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.

Keywords

References

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