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AN APPROXIMATE ANALYTICAL METHOD FOR VORTEX-LIFT AND CENTRE OE PRESSURE ON THE SLENDER WING
Yin Xieyuan
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1980, (1): 1 -6 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341