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Aerodynamic optimization design of large civil aircraft using pressure distribution inverse design method based on discrete adjoint
LIU Fengbo, JIANG Cheng, MA Tuliang, LIANG Yihua
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2020, (5): 623372 -623372 .  DOI: 10.7527/S1000-6893.2019.23372

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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