高超声速飞行器气动热关联换算方法研究
赵金山, 张志刚, 石义雷, 陈挺, 肖雨, 粟斯尧, 廖军好, 彭治雨

RESEARCH ON THE CONVERSION METHOD OF AEROHEATING ENVIRONMENT OF HYPERSONIC VEHICLE
Zhao Jinshan, Zhang Zhigang, Shi Yilei, Chen Ting, Xiao Yu, Su Siyao, Liao Junhao, Peng Zhiyu
表1 相同马赫数相同雷诺数情况下不同流场条件
Table 1 The typical flow field of the same Mach number and Reynolds number
State M Re · L-1 /m-1 T/K /Pa Tw/K
1 8.64 1.08 x 107 40 278.34 300
2 8.64 1.08 x 107 77 827.37 300
3 8.64 1.08 x 107 90 1056.45 300
4 8.64 1.08 x 107 200 3367.09 300
5 8.64 1.08 x 107 221 3879.77 300
6 19.97 1.82 x 107 221 2803.19 300