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Investigation of virtual flight testing technique based on 2.4 m transonic wind tunnel
ZHAO Zhongliang, WU Junqiang, LI Hao, ZHOU Weiqun, MAO Daiyong, YANG Haiyong
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2016, (2): 504 -512 .  DOI: 10.7527/S1000-6893.2015.0196

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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