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A NUMERICAL METHOD FOR ANALYZING THE NONLINEAR FLUTTER OF WINGS AT HIGH ANGLES OF ATTACK
Ye Zhengyin;Zhao Lingcheng
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1991, (10): 459 -463 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341