한국연소학회:학술대회논문집
- 한국연소학회 2000년도 제21회 KOSCO SYMPOSIUM 논문집
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- Pages.83-91
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- 2000
모델 스크램제트 연소기 내의 열적 질식 과정 수치 연구
Numerical Study of Thermal Choking Process in a Model SCRamjet Combustor
- 발행 : 2000.12.08
초록
A numerical study was carried out to investigate the 'unstart' process of thermally-choked combustion in model scramjet engines. The combustion mechanism of supersonic combustor will be compared with the experimental results obtained from the T3 free-piston shock tunnel at ANU (Australian National University) and the high enthalpy supersonic wind tunnel at UT (University of Tokyo). For the numerical simulation of supersonic combustion. multi-species Navier-Stokes equations were considered. and detailed chemistry reaction mechanism of