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Direct numerical simulation of shock wave/turbulent boundary layer interaction in hollow cylinder-flare configuration at Mach number 6
SUN Dong, LIU Pengxin, SHEN Pengfei, TONG Fulin, GUO Qilong
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2021, (12): 124681 -124681 .  DOI: 10.7527/S1000-6893.2020.24681

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341