THE COMPUTATION FOR 3-D FLOW FIELD IN RADIAL FLOW COMPRESSOR IMPELLER WITH SPUTTER BLADES CONSIDERING THE INFLUENCE OF UP AND DOWN STREAM

Abstract

Abstract: For a radial flow compupressor impeller with Spitter blades. The impeller blade passage was Prolonged by extending the stream surface of up and down stream and then making a long then passage of impeller blade. In this prolonged passage, three dimennsional Flow field was Solved by the Quasi-Orthogonal Surface. This method may be used for analyses of the flow field in this Kind of impeller with Prerotary flow and it may be used for analyses of varied working condition.

Key words: Alternating Direction Method of Multipliers, Incipient Fault, Sparse Low-rank Matrix, Taper Roller Bearings, Non-convex Regularization

Zhu Shican;Li Liangming. THE COMPUTATION FOR 3-D FLOW FIELD IN RADIAL FLOW COMPRESSOR IMPELLER WITH SPUTTER BLADES CONSIDERING THE INFLUENCE OF UP AND DOWN STREAM[J]. , 1986, 22(1): 61-69.

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THE COMPUTATION FOR 3-D FLOW FIELD IN RADIAL FLOW COMPRESSOR IMPELLER WITH SPUTTER BLADES CONSIDERING THE INFLUENCE OF UP AND DOWN STREAM

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