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)
Citation:
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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)
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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)
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)
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Study of Mach number effect in shock-wave/turbulent-boundary-layer interaction flow
- Available Online:
23 Dec 2022