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A NUMERICAL METHOD FOR COMPUTING THE AERODYNAMIC LOADS ON WINGS WITH SHARP-EDGE SEPARATIONS AT LARGE ANGLES OF ATTACK IN SUBCRITICAL TRANSONIC FLOWS
Ye Zhangyin;Yang Yongnian;Zhao Lingcheng
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1989, (10): 468 -473 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341