Radial inflow into the downstream cavity of a compressor stator well

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Scott, R M ^a   Childs, P R N ^a   Hills, N J ^a   Millward, J A ^b  

^a UNIVERSITY OF SUSSEX   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AXIAL FLOW TURBOMACHINERY; CENTRIFUGAL COMPRESSORS; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; FIGHTER AIRCRAFT; PRESSURE GRADIENT; STATORS; TURBOMACHINE BLADES;

AXIAL COMPRESSORS; COMMERCIAL CODES; COMPRESSOR PERFORMANCE; COMPRESSOR STATOR; DOWNSTREAM STATORS; EXPERIMENTAL RESEARCH; NOZZLE GUIDE VANES; THREE-DIMENSIONAL CFD MODEL;

SEALS;

EID: 84955272779     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0507     Document Type: Conference Paper

References (7)

1. Bayley, F.J., Conway, L., 1964, "Fluid Friction and Leakage Between a Stationary and Rotating Disc, " Journal of Mechanical Engineering Science, Vol.6, No.2, pp. 164-172.
2. Campobasso, M.S., Mattheiss, A., Wenger, U., Arnone, A., Boncinelli, P., 1999, "Complementary Use of CFD and Experimental Measurements to Assess the Impact of Shrouded and Cantilevered Stators in Axial Compressors, " ASME paper 99-GT-208.
3. Dixon, J.A., 1999, "Gas Turbine Critical Component Temperature Predictions for Fatigue Life and Integrity Considerations, " AIAA paper IS5/UNK05.
4. Freeman, C., 1985, "Effect of Tip Clearance Flow on Compressor Stability, " VKI Lecture series 1985-05.
5. Heidegger, N.J., Hall, E.J., Delaney, R.A., 1996, "Parameterised Study of High-Speed Compressor Seal Cavity Flow, " AIAA paper 96-2807.
6. Wellborn, S.R., Okiishi, T.H., 1998, "The Influence of Shrouded Stators Cavity Flows on Multistage Compressor Performance, " ASME paper 98-GT-12.
7. Wisler, D.C., 1988, "Advanced Compressor and Fan Systems, " GE Aircraft Engines, Cincinnati, OH, USA.