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Flow control technique for shock wave/turbulent boundary layer interactions
SHI Xiaotian, LYU Meng, ZHAO Yuan, TAO Shancong, HAO Le, YUAN Xiangjiang
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2022, (1): 625929 -625929 .  DOI: 10.7527/S1000-6893.2021.25929

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341