Rotating stall stability theory of the transonic axial compressors/fans

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作者
Yu, Wei-Wei [1 ]
Sun, Xiao-Feng [1 ]
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[1] School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
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Aerospace propulsion system - Rotating stall - Stability model - Winding number integral method;
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页码:1018 / 1027
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