Multiple segment parallel compressor model for circumferential flow distortion

Journal of Engineering for Gas Turbines and Power

Volumn 99, Issue 2, 1977, Pages 288-296

  Mazzawy, R S ^a  

^a PRATT AND WHITNEY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84997181835     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.3446288     Document Type: Article

References (9)

1. Greitzer, E. M., and Griswold, H. R, “Compressor-Diffuser Interaction With Circumferential Flow Distortion,”Project SQUID Workshop Proceedings, July 1974.
2. Plourde, G., and Stenning, A., “Attenuation of Circumferential Inlet Distortion in Multistage Compressors,” AIAA Paper 67-415, Aug. 1967.
3. Greitzer, E. M., “Upstream Circumferential Velocity Components in Nonuniform Compressor Flows,” to be submitted to JOURNAL OF ENGINEERING FOR POWER, TRANS. ASME.
4. McLafferty, G., “A Study of Perforation Configurations for Supersonic Diffusers,” UARL Report R-53372-7, Dec. 1950.
5. Emmons, H. W., Pearson, C. E., and Grant, H. P., “Compressor Surge and Stall Propagation,” TRANS. ASME, May 1955.
6. Roberts, F., Plourde, G., and Smakula, F., “Insights Into Axial Compressor Response to Distortion,” Fourth Propulsion Joint Specialist Conference, June 1968.
7. Nagano, S., Machida, Y., and Takata, H., “Dynamic Performance of Stalled Blade Rows,” Japan Society of Mechanical Engineers Paper JSME 11, Oct. 1971.
8. Mazzawy, R. S., Banks, G. A., and Weber, C. R., “Compressor Critical Response Time Determination Study,” TR AFAPL-TR76-45.
9. Pearson, C. E., “A Study of Surge in Compressors and Jet Engines,” Journal of the Aeronautical Sciences, Vol. 22, No. 1, Jan., 1955.