Details of axial-compressor shrouded stator cavity flows

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2001, Pages

  Wellborn, Steven R ^a  

^a ROLLS ROYCE CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; FLOW FIELDS; FLOW STRUCTURE;

CIRCUMFERENTIAL DIRECTION; CIRCUMFERENTIAL VARIATION; COMPLEX GEOMETRIES; MULTISTAGE COMPRESSOR; ROTATIONAL SPEED; TANGENTIAL VELOCITIES; VORTICAL FLOW STRUCTURES; VORTICAL STRUCTURES;

STATORS;

EID: 84875212431     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2001-GT-0495     Document Type: Conference Paper

References (14)

1. Bayley, E J. and Childs, R R. N., "Air Temperature Rises In Compressor and Turbine Stator Wells, " ASME Paper 94-GT-185, 1994.
2. Chew, J. W., Green, T., and Turner, A. B., "Rim Sealing of Rotor-Stator Wheel Spaces in the Presence of external Flow, " ASME Paper 94-GT-126, 1994.
3. Demargne, A. A. J. and Longley, J. R, "The Aerodynamic Interaction of Stator Shroud Leakage and Mainstream Flows in Compressors, " ASME Paper 2000-GT-570, 2000.
4. Hall, E. J., Heidegger, N. J., and Delaney, R. A., "Task 15-ADPAC User's Manual, " NASA Contract NAS3-27394, NASA CR 206600, January 1998.
5. Heidegge, ', N. J., Hall, E. J., and Delaney, R. A., "Parameterized Study of High-Speed Compressor Seal Cavity Flow, " AIAA Paper 96-2807, July 1996.
6. Jefferson, J. L. and Turner, R. C., "Some Shrouding and Tip Clearance Effects in Axial Flow Compressors, " International Ship Building Progress, Vol. 5, 1958, pp. 78-101.
7. Ozturk, H. K., Childs, R R. N., Turner, A. B., Hannis, J. M. and Turner, J. R., "A Three Dimensional Computational Study of Windage Heating Within an Axial Compressor Stator Well, " ASME Paper 98-GT-119, 1998.
8. Scott, R. M., Childs, P. R. N., Hills, N. J., and Milward, J. A., "Radial Inflow Into the Downstream Cavity of a Compressor Stator Well, " ASME Paper 2000-GT-507, 2000.
9. STAR CD Version 3. 05 Methodology Manual, adapco, 60 Broadhollow Raod, Melville, New York 11747 1998.
10. Wasserbauer, C. A., Weaver, H. F., and Senyitko, R. G., "NASA Low-Speed Axial Compressor for Fundamental Research, " NASA TM 4635, February 1995.
11. Wellborn, S. R. and Okiishi, T. H., "Effects of Shrouded Stator Cavity Flows on Multistage Axial Compressor Aerodynamic Pel'fornlance, " NASA CR 198536, October 1996.
12. Wellborn, S. R. and Okiishi, T. H., "The Influence of Shrouded Stator Cavity Flows on Multistage Compressor Performance, " Journal OfTurbomachinery, Vol. 122, April 1999.
13. Wellborn, S. R., Tolchinsky, I. and Okiishi, T. H., "Modeling Shrouded Stator Cavity Flows in Multistage Axial-Flow Compressors, " Journal Of Turbomachinery, Vol. 122, January 2000.
14. Wisler, D. C., Advanced Compressor and Fan Systems, GE Aircraft Engines, Cincinnati, Ohio, 1988. (Also 1986 Lecture to ASME Turbomachinery Institute, Ames, Iowa)