Simulating the multistage environment for single-stage compressor experiments

Journal of Turbomachinery

Volumn 118, Issue 4, 1996, Pages 706-716

  Place, J M M ^a   Howard, M A ^a   Cumpsty, N A ^b  

^a ROLLS ROYCE PLC   (United Kingdom)

^b UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSORS; FLOW;

EID: 0030478592     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2840926     Document Type: Article

References (18)

1. Bolger, J. J., 1994, private communication.
2. Camp, T. R., and Shin, H.-W., 1995, “Turbulence Intensity and Length Scale Measurements in Multistage Compressors,” ASME Journal of Turbomachinery, Vol. 117, pp. 38-46.
3. Cumpsty, N. A., 1989, Compressor Aerodynamics, Longman, United Kingdom, p. 168.
4. Cyrus, V., 1986, “Experimental Study of Three-Dimensional Flow in an Axial Compressor Stage,” ASME Paper No. 86-GT-118.
5. Cyrus, V., 1988, “Effect of the Inlet Velocity Profile in the Three-Dimensional Flow in a Rear Axial Compressor Stage,” ASME Journal of Turbomachinery, Vol. 110, pp. 434-440.
6. Denton, J. D., and Cumpsty, N. A., 1987, “Loss Mechanisms in Turbomachines,” presented at the Institute of Mechanical Engineers International Conference Turbomachinery—Efficiency Prediction and Improvement, Cambridge, Paper C260/87.
7. Goto, A., 1992, “Three-Dimensional Flow and Mixing in Axial Flow Compressor With Different Rotor Tip Clearances,” ASME Journal of Turbomachinery, Vol. 114, pp. 675-684.
8. Horlock, J. H., 1978, Actuator Disk Theory—Discontinuities in Thermo-Fluid Dynamics, McGraw-Hill, New York.
9. Howard, M. A., Ivey, P. C., Barton, J. P., and Young, K. F., 1993, “Endwall Effects at Two Tip Clearances in a Multi-stage Axial Flow Compressor With Controlled Diffusion Blading,” ASME Journal of Turbomachinery, Vol. 116, pp. 635-647.
10. Hunter, I. H., 1979, “Endwall Boundary Layer Flows and Losses in Axial Turbomachines,” PhD Thesis, University of Cambridge, United Kingdom.
11. Lambie, D., 1989, “Inlet Distortion and Turbofan Engines,” PhD Thesis, University of Cambridge, United Kingdom.
12. Lewis, K. L., 1993, “The Aerodynamics of Shrouded Multi-stage Turbines,” PhD thesis, University of Cambridge, United Kingdom.
13. Li, Y. S., and Cumpsty, N. A., 1991, “Mixing in Axial Compressors: Part II— Measurements in a Single-Stage Compressor and a Duct,” ASME Journal of Turbomachinery, Vol. 113, pp. 166-174.
14. McDougall, N. M., 1988, “Stall Inception in Axial Compressors,” PhD Thesis, University of Cambridge, United Kingdom.
15. Place, J. M. M., 1995, “Three-Dimensional Flow in Axial Compressors,” PhD Thesis, University of Cambridge (to be submitted).
16. Savin, N. M., 1993, private communication.
17. Smith, L. H., 1970, “Casing Boundary Layers in Multistage Axial-Flow Compressors,” Flow Research on Blading, L. S. Dzung, ed., Elsevier, pp. 275-303.
18. Wisler, D. C., 1980, “Core Compressor Exit Stage Study, Vol. II—Data and Performance Report for the Baseline Configuration,” NASA Report No. CR-159498, Nov.