On the use of atmospheric boundary conditions for axial-flow compressor stall simulations

Journal of Turbomachinery

Volumn 127, Issue 2, 2005, Pages 349-351

  Vahdati, M ^a   Sayma, A I ^a   Freeman, C ^b   Imregun, M ^a  

^a IMPERIAL COLLEGE LONDON   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; HYSTERESIS; INTAKE SYSTEMS; NOZZLES;

AXIAL-FLOW COMPRESSORS; COMPUTATIONAL DOMAINS; HYSTERESIS LOOP BEHAVIOR; VARIABLE NOZZLE DOWNSTREAM;

AXIAL FLOW TURBOMACHINERY;

AERODYNAMICS;

EID: 21444450186     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1861912     Document Type: Article

References (6)

1. Freeman, C., 1992, "The Effect of Aircraft Inlets on the Behavior of Aero Engine Axial Flow Compressors," VKI Lecture Series, Axial Flow Compressors, 1992-02
2. Day, I. J., 1992, "Stall and Surge in Axial Flow Compressors," VKI Lecture Series, Axial Flow Compressors, 1992-02.
3. Longley, J. P., and Hynes, T. P., 1990, "Stability of Flow Through Multi-stage Axial Compressors," ASME J. Turbomach., 112(1), pp. 126-132.
4. Weigl, H. J., Paduano, J. D., Fréchette, L. G., Epstein, A. H., Greitzer, E. M., Bright, M. M., and Strazisar, A. J., 1998, "Active Stabilization of Rotating Stall and Surge in a Transonic Single-Stage Compressor," ASME J. Turbomach., 120(4), pp. 625-636.
5. Moore, F., and Greitzer, E. M., 1986, "A Theory of Post-Stall Transients in Axial Compressors - Part I: Development of the Equations," ASME J. Eng. Gas Turbines Power, 108(1), pp. 371-379.
6. Sayma, A. I., Vahdati, M., Sbardella, L., and Imregun, M., 2000, "Modeling of 3D Viscous Compressible Turbomachinery Flows using Unstructured Hybrid Grids," AIAA J., 38(6), pp. 945-954.