Investigation of flow mechanisms in multistage axial-flow compressor

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Department of Thermal Engineering, Tsinghua University, Beijing 100084, China ^{[1
]}

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Kung Cheng Je Wu Li Hsueh Pao | 2007年 / SUPPL. 1卷 / 133-135期

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Compressors;

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引用

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[31] Study of the clearance leakage flow characteristics of a transonic axial-flow compressor
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[32] CONTRIBUTION TO CALCULATE PERFORMANCE OF MULTISTAGE AXIAL-FLOW COMPRESSORS
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ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1977, 1 (02): : 116 - 122
[33] SOUND-PROPAGATION IN MULTISTAGE AXIAL-FLOW TURBOMACHINES
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[34] Blade Design of Multistage Axial-Flow Compressors.
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[35] THE GAS BENDING STRESS ON A BLADE IN AN AXIAL-FLOW COMPRESSOR
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JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (05): : 357 - 359
[36] Experimental application of extremum seeking on an axial-flow compressor
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[37] STABILITY OF AN AXIAL-FLOW COMPRESSOR WITH STEADY INLET CONDITIONS
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[38] UNSTEADY TRANSONIC-FLOWS IN AN AXIAL-FLOW COMPRESSOR
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[39] A NEW METHOD FOR PREDICTING PERFORMANCE OF AXIAL-FLOW COMPRESSOR
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[40] BIFURCATION-ANALYSIS OF AXIAL-FLOW COMPRESSOR STABILITY
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SIAM JOURNAL ON APPLIED MATHEMATICS, 1990, 50 (05) : 1232 - 1253

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