An investigation of the effect of cascade area ratios on transonic compressor performance

Journal of Turbomachinery

Volumn 118, Issue 4, 1996, Pages 760-770

  Wadia, A R ^a   Copenhaver, W W ^b  

^a GE AVIATION   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 4243125711     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2840932     Document Type: Article

References (12)

1. Copenhaver, W. W., Hah, C, and Puterbaugh, S. L., 1993, “Three-Dimensional Flow Phenomena in a Transonic, High-Through-Flow, Axial-Flow Compressor Stage,” ASME Journal of Turbomachinery, Vol. 115, pp. 240-248.
2. Hah, C., and Puterbaugh, S. L., 1990, “A Critical Evaluation of a ThreeDimensional Navier-Stokes Method as a Tool to Calculate Transonic Flows Inside a Low-Aspect-Ratio Compressor,” AGARD Conference Proceedings 510, CFD Techniques for Propulsion Applications, pp. 10-1-10-14.
3. Jennions, I. K., and Turner, M. G., 1993a, “Three-Dimensional Navier—Stokes Computations of Transonic Fan Flow Including a Novel Implementation of an Implicit k-e Turbulence Model,” ASME Journal of Turbomachinery, Vol. 115, pp. 249-261.
4. Jennions, I. K., and Turner, M. G., 1993b, “Three-Dimensional Navier-Stokes Computations of Transonic Fan Flow Using an Explicit-Flow Solver and an Implicit k-e Solver,” ASME Journal of Turbomachinery, Vol. 115, pp. 261-272.
5. Kantrowitz, A., 1950, “The Supersonic Axial Flow Compressor,” NACA Report 974, 1950.
6. Klapproth, J. F., 1961, “A Review of Supersonic Compressor Development,” ASME Journal of Engineering for Power, Vol. 83, No. 2, pp. 258-268.
7. Law, C. H., and Wadia, A. R., 1993, “Low Aspect Ratio Transonic Rotors: Part 1—Baseline Design and Performance,” ASME Journal of Turbomachinery, Vol. 115, No. 2, pp. 218-225.
8. Parker, D. E., and Simonson, M. R., 1982, “Transonic Fan/Compressor Rotor Design Study, Vols. IV, V, VI,” AFWAL-TR-82-2017.
9. Sellin, M. D., Puterbaugh, S. L., and Copenhaver, W. W., 1993, “Tip Shock Structures in Transonic Compressor Rotors,” AIAA Paper No. 93-1869.
10. Smith, L. H., and Yeh, H., 1962, “Sweep and Dihedral Effects in Axial Flow Turbomachinery,” ASME Paper No. 62-WA-102.
11. Wadia, A. R., and Law, C. H., 1993, “Low Aspect Ratio Transonic Rotors: Part 2—Influence of Location of Maximum Thickness on Transonic Compressor Performance,” ASME Journal of Turbomachinery, Vol. 115, pp. 226-239.
12. Wennerstrom, A. J., 1994, “Experimental Study of a High-Through-Flow Transonic Axial Compressor Stage,” ASME Journal of Engineering for Gas Turbines and Power, Vol. 106, pp. 552-560.