引用本文: | 吴正园, 高振勋, 陈新民, 等 . 激波与湍流边界层干扰流动的马赫数效应研究[J]. 北京航空航天大学学报. doi: 10.13700/j.bh.1001-5965.2022.0857 |
Citation: | WU Zheng-yuan, GAO Zhen-xun, CHEN Xin-min, et al. Study of Mach number effect in shock-wave/turbulent-boundary-layer interaction flow[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2022.0857(in Chinese) |