马赫6柱-裙构型激波/湍流边界层干扰摩阻统计特性
沈鹏飞, 刘朋欣, 孙东, 袁先旭
Statistical characteristics of skin friction of shock wave/turbulent boundary layer interaction in hollow cylinder-flare configuration at Mach 6
SHEN Pengfei, LIU Pengxin, SUN Dong, YUAN Xianxu
航空学报 . 2022, (1): 626005 -626005 .  DOI: 10.7527/S1000-6893.2021.26005