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Implementation of an Improved Unsteady Vortex Lattice Method for Flexible Flapping-wing Aerodynamic Computation
He Honglin;Zhou Xiang
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2010, (6): 1121 -1126 . 

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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