Rotating stall control in a high-speed stage with inlet distortion: Part II—Circumferential distortion

Journal of Turbomachinery

Volumn 121, Issue 3, 1999, Pages 517-524

  Spakovszky, Z S ^a   Van Schalkwyk, C M ^b   Weigl, H J ^a   Pacluano, J D ^a   Suder, K L ^c   Bright, M M ^c  

^a Massachusetts Institute of Technology   (United States)

^b SCIENTIFIC SYSTEMS COMPANY INC   (United States)

^c NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; FLOW CONTROL; HARMONIC ANALYSIS; INTAKE SYSTEMS; MODAL ANALYSIS; PARAMETER ESTIMATION; RADIAL FLOW; ROTATING DISKS; SYSTEM STABILITY; TRANSFER FUNCTIONS;

AXIAL FLOW COMPRESSORS; INLET DISTORTION; MOORE-GREITZER MODE; PRESSURE PERTURBATIONS; ROTATING STALL CONTROL;

AXIAL FLOW TURBOMACHINERY;

AXIAL FLOW COMPRESSOR; CONTROL METHOD; FLOW; INLET; STALL;

EID: 0032723966     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841346     Document Type: Article

References (20)

1. Bemdt, R., Weigl, H., Paduano, J., and Epstein, A., 1995, “Experimental Techniques for Actuation, Sensing, and Measurement of Rotating Stall Dynamics in High Speed Engines,” in: J. D. Paduano, ed., Sensing, Actuation, and Control in Aeropro-pulsion, Vol. 2492, SPIE.
2. Bonnaure, L., 1991, “Modelling High Speed Multistage Compressor Stability,” Master’s thesis, Department of Aeronautics and Astronautics, MIT.
3. Feulner, M., Hendricks, G., and Paduano, J., 1994, “Modeling for Control of Rotating Stall in High Speed Multi-Stage Axial Compressors,” ASME Paper No. 94-GT-292.
4. Haynes, J., Hendricks, G., and Epstein, A., 1994, “Active Stabilization of Rotating Stall in a Three-Stage Axial Compressor,” ASME Journal of Turbomachinery, Vol. 116, pp. 226-239.
5. Hendricks, G., Bonnaure, L., Longley, J., Greitzer, E., and Epstein, A., 1993, “Analysis of Rotating Stall Onset in High Speed Axial Flow Compressors,” Paper No. AIAA-93-2233.
6. Hynes, T., and Greitzer, E., 1987, “A Method for Assessing Effects of Circumferential Flow Distortion on Compressor Stability,” ASME Journal of Turbomachinery, Vol. 109, pp. 371-379.
7. Jacques, R., 1994, “On-Line System Identification and Control Design for Flexible Structures,” Ph.D. thesis, Department of Aeronautics and Astronautics, MIT.
8. Koch, C. C., 1970, “Experimental Evaluation of Outer Case Blowing or Bleeding of a Single-Stage Axial Flow Compressor,” Tech. Rep. CR-54592, NASA.
9. Ljung, L., 1987, System Identification: Theory for the User, Prentice-Hall, Inc.
10. Longley, J., and Greitzer, E., 1992, “Inlet Distortion Effects in Aircraft Propulsion System Integration,” Steady and Transient Performance Prediction of Gas Turbine Engines, AGARD-LS-183, pp. 6-1-6-18.
11. Moore, F., and Greitzer, E., 1986, “A Theory of Post-Stall Transients in Axial Compressors: Part I—Development of the Equations,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 108, pp. 68-76.
12. Paduano, J., Epstein, A., Valavani, L., Longley, J., Greitzer, E., and Guenette, G., 1993, “Active Control of Rotating Stall in a Low-Speed Axial Compressors,” ASME Journal of Turbomachinery, Vol. 115, pp. 48-56.
13. Reid, L., and Moore, D., 1978, “Performance of Single-Stage Axial-Flow Transonic Compressor With Rotor and Stator Aspect Ratios of 1.19 and 1.26, Respectively, and With Design Pressure Ratio 1.82,” Tech. Rep. TP-1338, NASA.
14. Spakovszky, Z., 1999, “Active Control of Rotating Stall in a Transonic Compressor Stage With Inlet Distortion,” Master’s thesis, Department of Aeronautics and Astronautics, MIT.
15. Spakovszky, Z., Weigl, H., Paduano, J., Van Schalkwyk, C., Suder, K., and Bright, M., 1999, “Rotating Stall Control in a High-Speed Stage With Inlet Distortion, Part I—Radial Distortion,” ASME Journal of Turbomachinery, Vol. 121, this issue, pp. 508-514.
16. Van Schalkwyk, C., 1996, “Active Control of Rotating Stall With Inlet Distortion,” Ph.D. thesis, Department of Aeronautics and Astronautics, MIT; also available as Gas Turbine Lab Report #222.
17. Van Schalkwyk, C., Paduano, J., Greitzer, E., and Epstein, A., 1998, “Active Stabilization of Axial Compressors With Circumferential Inlet Distortion,” ASME Journal of Turbomachinery, Vol. 120, pp. 431-439.
18. Weigl, H., Paduano, J., Fréchette, L., Epstein, A., and Greitzer, E., 1998, “Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor,” ASME Journal of Turbomachinery, Vol. 120, pp. 625-636.
19. Weigl, H. J., 1997, “Active Stabilization of Rotating Stall and Surge in a Transonic Single Stage Axial Compressor,” Ph.D. thesis, Department of Aeronautics and Astronautics, MIT.
20. Williams, D., 1991, “Engine Compatibility,” Tech. rep., Rolls-Royce pic.