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A NEW METHOD FOR PREDICTING THE END WALL BOUNDARY LAYERS AND THE BLADE FORCE DEFECTS iNSIDE THE PASSAGE OF AXIAL COMPRESSOR CASCADES
Wu Hu;Chen Fu-qun;Liu Song-ling;Huang Zhi-tao
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1992, (1): 48 -56 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341