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FLUX-SPLITTING IMPLICIT FINITE VOLUME METHOD FOR THE CALCULATION OF THE SUPERSONIC FLOW WITH STRONG INTERACTION OF A JET
Wang Zhenghua;Wang Chengyao
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1996, (1): 1 -8 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341