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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1995, Vol. 16 ›› Issue (1): 43-47.
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Chen Yuanxian, Lai Bin
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Abstract: The three-dimensional flow field of a centrifugal impeller for aircraft cooling turbine is computed with quasi-orthogonal surface method in cluding the influence of upstream and downstream conditions.The calculated flow field of the centrifugal impeller and the improvement of the blade shape are discussed.
Key words: cent rifugal compressors, three dimensional flow, impellers
CLC Number:
V24511
Chen Yuanxian;Lai Bin. COMPUTATION OF THREE-DIMENSIONAL FLOW FIELD IN A CENTRIFUGAL IMPELLER[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(1): 43-47.
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