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237篇 您的检索式:作者名="Greitzer"
    题名 作者 年代 出处 被引量
1Predition of Compressor Performance in Rotating Stall显示文摘Day I J Greitzer E M Cumpsty N A 1978Journal of Engineering for Power1978,100,:2
2Effects of inlet flow field conditions on the performance of centrifugal compressor diffusers:straight channel diffuser显示文摘Deniz S Greitzer E M Cumpsty N A 2000ASME Journal of Turbomachinery2000,122,1:1
3A fundamental criterion for the application of rotor casing treatment显示文摘Greitzer E M Nikkanen J P Haddad D E 1979Journal of Fluids Engineering1979,101,2:1
4Surge and rotating stall in axial flow compressors显示文摘GREITZER E M 1976Journal of Engineering for Power1976,,4:1
5NumericalSimulation of Compressor Endwall and CasingTreatment Flow Phenomena 显示文摘Crook A J Greitzer E M Tan C S 1993ASME Journal ofTurbomachinery1993,115,3:1
6The stability of pumping systems-1980 freeman scholar lecture 显示文摘Greitzer E M 1981ASME Journal of Fluids En- gineering1981,103,6:1
7M, 'Surge and Rotating stall in Axial Flow Compressors 显示文摘Greitzer E 1976Part I: Theoretical Compression System Model' ASME Jourmal of Engineering For Power Vol 981976,,:1
8Effect of compressor hub treat-ment on stator stall margin and performance 显示文摘Cheng P Prell M E Greitzer E M 1984Journal of Air- craft1984,21,7:1
9A theory of post stall ransients in axial compressor system,Part I Development of equations, Part I1 Application显示文摘Moore F K Greitzer E M 1986Journal of Turbomachinery1986,108,68:1
10Effect of Slotted Hub and Casing Treatment on Compressor Endwall Flowfield显示文摘Johnson M C Greitzer E M 1987ASME Journal of Turbomachinery1987,109,2:1
11Prediction of Com- pressor Performance in Rotating Stall 显示文摘Day I J Greitzer E M Cumpsty N A 1978ASME Journal of Turbomaehinery1978,100,1:1
12Numerical Simulation of Compressor Endwall and Casing Treatment Flow Phenomena 显示文摘Crook A J Greitzer E M Tan C S Adamczyk J J 1993ASME Journal of Turbomachinery1993,115,:1
13Compressor-diffuser interaction with circumferential flow distortion显示文摘 1979Journal of Mechanical Engineering Sciences,1979,18,2:1
14The role of tip clearance in high-speed fan stall 显示文摘ADAMCZYK J J CELESTINA M L GREITZER E M 1993Journal of Turhomachinery1993,115,1:1
15Rotating Waves as a Stall Inception Indication in Axial Compressors 显示文摘Granier V H Epstein A H Greitzer E M 1991ASME Journal of Turbomachinery1991,113,2:1
16Similarity analysis of compressor tip clearance flow structure显示文摘Chen G T Greitzer E M Tan C S 1991ASME Journal of Turbomachinery1991,113,2:1
17Active Suppression of Aerodynamic Instabilities in Turbo- machineryies显示文摘Epstein A H Ffowcs W J E Greitzer E M 1989Journal of Propulsion and Power1989,5,:1
18Criteria for Spike Initi- ated Rotating Stall 显示文摘Vo H D Tan C S Greitzer E M 2008Journal of Turbomachinery2008,130,:1
19A Theory of Poststall Transients in Axial Compressors--part I: Develop- ment of Equations显示文摘Moore F K Greitzer E M 1986Journal of Turbomachinery1986,108,:1
20Criteria for Spike Ini- tiated Stall 显示文摘Vo H D Tan C S Greitzer E M 2008ASME Journal of Turbomachinery2008,130,1:1
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