Short length-scale rotating stall inception in a transonic axial compressor - Criteria and mechanisms

Proceedings of the ASME Turbo Expo

Volumn 6 PART A, Issue , 2006, Pages 61-70

  Hah, Chunill ^a   Bergner, Jörg ^b   Schiffer, Heinz Peter ^b  

^a NASA GLENN RESEARCH CENTER   (United States)

^b DARMSTADT UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW MECHANISM; PASSAGE SHOCK; ROTATING STALL; TRANSONIC AXIAL COMPRESSOR;

COMPUTER SIMULATION; NAVIER STOKES EQUATIONS; OSCILLATORS (MECHANICAL); PRESSURE TRANSDUCERS; ROTATIONAL FLOW; VORTEX FLOW;

COMPRESSORS;

EID: 33750872522     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2006-90045     Document Type: Conference Paper

References (16)

1. Bergner, J., Hennecke, D. K., and Hah, C., 2005, "Tip-Clearance Variations of an Axial High-Speed Single-Stage Transonic Compressor," ISABE Paper ISABE-2005-1096.
2. Camp, T. R. and Day, I. J., 1998, "A Study of Spike and Modal Stall Phenomena in a Low-Speed Axial Compressor," ASME Journal of Turbomachinery, Vol. 120, pp.393-401.
3. Germano, M., Piomelli, U., Moin, P., and Cabot, W. H., 1991, "A Dynamic Subgrid -Scale Eddy-Viscosity Model," Journal of Fluid Mechanics, Vol. A3, pp. 170-176.
4. Gong, Y., Tan, C. S., Gordon, K A., and Greitzer, E. M., 1999, "A Computational Model for Short Wavelength Stall Inception and Development in Multi-Stage Compressors," ASME Journal of Turbomachinery, Vol. 121, pp.726-734.
5. Hah, C. and Rabe, D. C., 2001, 'Role of Tip Clearance Flows on Flow Instability in Axial Flow Compressors," ISABE Paper 2001-1223.
6. Hah, C., Rabe, D. C., and Wadia, A. R., 2004, "Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor," ASME Paper GT2004-53867.
7. Hah, C. and Wennerstrom, A. J., 1991, Three-Dimensional Flow Fields Inside a Transonic Compressor with Swept Blades," ASME Journal of Turbomachinery, Vol. 113, No. 1, pp. 241-251.
8. He, L. and Ismael, J. O., 1997, "Computations of Blade Row Stall Inception in Transonic Flows," ISABE Proceedings, pp.697-707.
9. Hoying, D. A., Tan, C. S., Vo, H. D., and Greitzer, E. M., 1998, "Role of Blade Passage Flow Structures in Axial Compressor Rotating Stall Inception," ASME Paper 98-GT-588.
10. Hoffmann W. H. and Ballmann, J., 2003, 'Some Aspects of Tip Vortex Behavior in a Transonic Turbocompressor," ISABE Paper 2003-1223.
11. Moore, F. K. and Greitzer, E. M., 1986a, "A Theory of Post-Stall Transients in Axial Compression Systems: Part 1 -Development Equations," ASME Journal of Engineering for Gas Turbines and Power, Vol. 108, pp. 68-76.
12. Moore, F. K. and Greitzer, E. M., 1986b, "A Theory of Post-Stall Transients in Axial Compression Systems: Part 2 -Application," ASME Journal of Engineering for Gas Turbines and Power, Vol. 108, pp. 231-239.
13. Outa, E., Kato, D., and Chiba, K., 1994, "A N-S Simulation of Stall Cell Behavior in a 2-D Compressor Rotor-Stator System at Various Loads," ASME Paper 94-GT-257.
14. Saxer-Felici, H. M., Saxer, A. P., Inderbitzin, A., and Gyarmathy, G., 1998, "Prediction and Measurement of Rotating Stall Cells in an Axial Compressor," ASME Paper 98-GT-67.
15. Van Zante, D. E., Strazisar, A. J., Wood, J. R., Hathaway, M. D., Okiishi, T. H., 2000, 'Recommendations for Achieving Accurate Numerical Simulation of the Tip Clearance Flows in Transonic Compressor Rotors," ASME Journal of Turbomachinery, Vol. 122, pp. 733-742.
16. Vo, H. D., Tan, C. S., and Greitzer, E. M., 2005, 'Criteria for Spike Initiated Rotatin g Stall," ASME Paper GT2005-68374.