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AN IMPROVED THREE DIMENSIONAL MODEL FOR THE PREDICTION OF SHOCK LOSSES IN COMPRESSOR BLADE ROWS
Zhang Yangjun;Tao Deping;Zhou Sheng
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1995, (1): 105 -109 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341