Effects of stator pressure field on upstream rotor performance

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1999, Pages

  Graf, M B ^a   Greitzer, E M ^b   Marble, F E ^c   Sharma, O P ^d  

^a Mars and Company   (United States)

^b MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

^c CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^d UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; FLOW OF FLUIDS; GAS TURBINES; HIGH PRESSURE EFFECTS; LEAKAGE (FLUID); NAVIER STOKES EQUATIONS; STATORS; STEADY FLOW; VORTEX FLOW;

DETERMINISTIC STRESS; HIGH PRESSURE COMPRESSOR; OPERATING POINTS; REYNOLDS - AVERAGED NAVIER-STOKES; ROTOR PERFORMANCE; ROTOR-STATOR INTERACTIONS; STEADY-FLOW MODEL; TIP LEAKAGE VORTEX;

ROTORS (WINDINGS);

EID: 84928532138     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-099     Document Type: Conference Paper

References (23)

1. Smith, L. H., Jr., "The effect of tip clearance on the peak pressure rise of axial-flow fans and compressors," ASME Symposium on Stall, 1958, 149-152.
2. Koch, C. C., "Stalling pressure rise capability of axial flow compressor stages," ASME J Eng. Power, 1981, vol. 103, 645-656.
3. Baghdadi, S., "Modeling tip clearance effects in multistage axial compressors," ASME Paper, 95-GT-291, 1995.
4. Adamczylc, J. J., Greitzer, E. M., Strazisar, A. J., "Recommendations from the NASA workshop on unsteady flows in turbomachines: potential benefits, present status, future research," Summary of workshop held at NASA Lewis Research Center, May 20-21, 1992.
5. Greitzer, E. M., Tan, C. S., Wisler, D. C., Adamczyk, J. J., Strazisar, A. J., "Unsteady flow in turbomachines: where's the beef?," A SME Unsteady Flows in Aeropropulsion, 1994, AD-vol. 40, 1-11.
6. Lejambre, C. R., Zacharias, R. M., Biederman, B. P., Gleixner, A. J., Yetka, C. J., "Development and application of a multistage Navier-Stokes solver, Part II: Application to a high pressure compressor design," ASME Paper, 95-GT-342, 1995.
7. Davis, R. L., Shang, T., Buteau, J. D., Ni, R-H. R., "Prediction of 3-D unsteady flow in multi-stage turbomachinery using an implicit dual time-stepping approach," AIAA Paper, 96-2565, 1996.
8. Rhie, C. M., Gleixner, A. J., Spear, D. A., Fischberg, C. J., Zacharias, R. M., "Development and application of a multistage Navier-Stokes solver, Part I: Multistage modeling using bodyforces and deterministic stresses," ASME Paper, 95-GT-342, 1995.
9. Ni, R-H. R., Bogoian, J. C., "Prediction of 3D multistage turbine flow field using a multiple-grid Euler solver," AIAA Paper, 89-0203, 1989.
10. Ni, R-H. R., "A multiple-grid scheme for solving the Euler equations," AIAA Paper, 81-1025, 1981.
11. Baldwin, B., Lomax, H., "Thin layer approximation and algebraic model for separated turbulent flows," AIAA Paper, 78-0257, 1978.
12. Jameson, A., Schmidt, W., Turkel. E., "Numerical solution of the Euler equations by finite volume methods using Runge-Kutta time stepping schemes," A1AA Paper, 81-1259, 1981.
13. Dawes, W. N., "Toward improved throughflow capability: The use of three-dimensional viscous flow solvers in a multistage environment," ASME J. Turbomachinery, 1992, vol. 114, 8-17.
14. Saxer, A. P., "A numerical analysis of 3-D inviscid stator/rotor interactions using non-reflecting boundary conditions," Massachusetts Institution of Technology, Department of Aeronautics and Astronautics, Gas Turbine Laboratory Report No. 209.
15. Martinelli, L., Jameson, A., "Validation of a multigrid method for the Reynolds Avenged equations," AIAA Paper, 88-0414, 1988.
16. Adamczyk, J., "Model equation for simulating flows in multistage turbomachinery," ASME Paper, 85-0T-226, 1985.
17. Graf, M.B., "Effects of stator pressure field on upstream rotor performance," Doctoral Thesis, Massachusetts Institute of Technology, Department of Mechanical Engineering, 1996.
18. Khalid, S. A., "The effects of tip clearance on axial compressor pressure rise," Doctoral Thesis, Massachusetts Institute of Technology, Department of Mechanical Engineering, 1995.
19. Adamczyk, J. J., Celestine, M. L., Greitzer, E. M., "The role of tip clearance in high-speed fan stall," ASME J Turbomachinery, 1993, vol. 115,28-38.
20. Khalsa, A. S., "Endwall blockage in axial compressors," Doctoral Thesis, Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 1996.
21. Storer, J. A., Cumpsty, N. A., "An approximate analysis and prediction method for tip clearance loss in axial compressors," ASME Paper, 93-GT-140, 1993.
22. Denton, J. D., "Loss mechanisms in turbomachines," ASME J. Turbomachinery, 1993, vol. 115, 621-656.
23. Graf, M. B., Sharma, O. P., "Effects of downstream stator pressure field on upstream rotor performance," ASME Paper, 96-GT-507, 1996.