Numerical Study of Thermal Choking Process in a Model SCRamjet Combustor
모델 스크램제트 연소기 내의 열적 질식 과정 수치 연구
- Published : 2000.12.08
Abstract
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