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압력 조건과 기저 온도 조건에 따른 기저 열전달률 계산
김재관(J.G. Kim),이준우(J.W. Lee),최중근(J.K. Choi),김규홍(K.H. Kim) 한국전산유체공학회 2011 한국전산유체공학회 학술대회논문집 Vol.2011 No.5
Numerical study was conducted to simulate the heat transfer on the real launch vehicle base. Three different base temperatures were chosen, to simulate the heat accumulation on the base. Moreover, six different pressure ratio conditions were used to express the different air conditions. As a result, the table that can used to estimate the base heat flux along the base temperature and pressure condition was made.