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Wall Temperature Effect on Transition Flow and Separated Flow in Hypersonic Flow Around a Blunt Double Wedge
SHANG Qing, CHEN Lin, LI Xue, YUAN Xiangjiang
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2014, (11): 2958 -2969 .  DOI: 10.7527/S1000-6893.2014.0162

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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