Comparison of the AUSM+ and H-Cuspschemes for turbomachinery applications

16th AIAA Computational Fluid Dynamics Conference

Volumn , Issue , 2003, Pages

  Chima, R V ^a   Liou, M S ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ARTIFICIAL VISCOSITY; CONVERGENCE RATES; EXIT DISTRIBUTION; NUMERICAL PROBLEMS; PREDICTIVE CAPABILITIES; SUPERSONIC COMPRESSORS; TRANSONIC TURBINE; TURBOMACHINERY APPLICATIONS;

COAL FUELED GAS TURBINES; NASA; TURBINES;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84897708411     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (30)

1. Dunham, J., ed. "CFD Validation for Propulsion Sys tem Components," AGARD Advisory Report 355, AGARD, Nellie-Sur-Seine, France, May, 1998.
2. Dunham, J., and Meauzé, "An AGARD Working Group Study of 3-D Navier-Stokes Codes Applied to Single Turbomachinery Blade Rows," ASME Paper 98- GT-50, June 1998.
3. Reid, L., and Moore, R. D., "Design and Overall Performance of Four Highly-Loaded, High-Speed Inlet Stages for an Advanced, High-Pressure-Ratio Core Compressor," NASA TP-1337, 1978.
4. Reid, L., and Moore, R. D., "Experimental Study of Low Aspect Ratio Compressor Blading," ASME Paper 80-GT-6, Mar. 1980.
5. Tweedt, D.L., Chima, R. V., and Turkel, E. "PrecondiTioning for Numerical Simulation of Low Mach Number Three-Dimensional Viscous Turbomachinery Flows," AIAA Paper 97-1828, June, 1997.
6. Chima, R. V., "A k-w Turbulence Model for Quasi- Three-Dimensional Turbomachinery Flows," AIAA Paper 96-0248, 1995. Also NASA TM-107051.
7. Jameson, A., Schmidt, W., and Turkel, E., "Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes," AIAA Paper 81-1259, June 1981.
8. Martinelli, L., and Jameson, A., "Validation of a Multi- grid Method for the Reynolds Averaged Equations," AIAA Paper 88-0414, Jan. 1988.
9. Kunz, R. F., and Lakshminarayana, B. "Explicit Navier-Stokes Computation of Cascade Flows Using the k-e Turbulence Model," AIAA J., Vol. 30, No. 1, Jan. 1992, pp. 13-22.
10. Tatsumi, S., Martinelli, L., and Jameson, A., "Design, Implementation, and Validation of Flux Limited Schemes for the Solution of the Compressible Navier- Stokes Equations," AIAA Paper 94-0647, Jan. 1994.
11. Tatsumi, S., Martinelli, L., and Jameson, A., "A New High Resolution Scheme for Compressible Viscous Flows with Shocks," AIAA Paper 95-0466, Jan. 1995.
12. Liou, M.-S., and Steffen, Jr., C. J., "A New Flux Split ting Scheme," J. Computational Physics, Vol. 107, No. 1, July 1993, pp. 23-39. ALSO NASA TM 104404, May 1991.
13. +," J. Computational Physics, Vol. 129, 1996, pp. 364-382. Also NASA TM 106524, March 1994.
14. Liou, M.-S., and Edwards, J. R., "Numerical Speed of Sound and its Application to Schemes for all Speeds," AIAA Paper 99-3268-CP, 14th AIAA CFD Conference, 1999. Also NASA TM-1999-209286, June 1999.
15. Liou, M.-S., "Ten Years in the Making - AUSM-Fam-ily," AIAA Paper 2001-2521, June 2001.
16. Chima, Rodrick V., "Explicit Multigrid Algorithm for Quasi-Three-Dimensional Viscous Flows in Turboma- chinery," AIAA Journal of Propulsion and Power, Vol. 3, No. 5, Sept.-Oct. 1987, pp. 397-405.
17. Chima, R. V., "Viscous Three-Dimensional Calculations of Transonic Fan Performance," in CFD Tech niques for Propulsion Applications, AGARD Conference Proceedings No. CP-510, AGARD, Neuilly- Sur-Seine, France, Feb. 1992, pp 21-1 to 21-19. Also NASA TM-103800.
18. Chima, Rodrick V., "Calculation of Tip Clearance Effects in a Transonic Compressor Rotor," ASME Paper 96-GT-114, June 1996. Also NASA TM-107216.
19. Chima, Rodrick V., "Calculation of Multistage Turbo- machinery Using Steady Characteristic Boundary Conditions," AIAA Paper 9800968, Jan. 1998. Also NASA TM-1998-206613.
20. Baldwin, B. S., and Lomax, H., "Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, Jan. 1978.
21. Wilcox, D.C., Turbulence Modeling for CFD, DCW Industries, Inc., La Canada, CA, 1994.
22. Menter, F. R., "Improved Two-Equation k-w Turbu lence Model for Aerodynamic Flows,"NASA TM- 103975, Oct. 1992.
23. Swanson, R. C., Radespiel, R., and Turkel, E., "Comparison of Several Dissipation Algorithms for Central Difference Schemes,"NASA-CR-201726, Aug. 1997. Also ICASE-97-40.
24. van Albada, G. D., van Leer, B., and Roberts, W. W., "A Comparative Study of Numerical Methods in Cosmic Gas Dynamics,"ICASE Report No. 81-84, Aug. 1981.
25. Arts, T., Lambert de Rouvroit, M., and Rutherford, A.W., "Aero-Thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade,"von Karman Institute Technical Note 174, Sept. 1990.
26. Goldman, L. J., and McLallin, K. L., "Cold-Air Annular-Cascade Investigation of Aerodynamic Performance of Core-Engine-Cooled Turbine Vanes. I: Solid- Vane Performance and Facility Description,"NASA TM X-3224, 1975.
27. Suder, K.L., and Celestina, M. L., "Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor,"NASA TM- 106711, 1994.
28. Suder, K. L., Chima, R. V., Strazisar, A. J., and Roberts, W.B., "The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor," ASME J. Turbomachinery, Vol. 117, Oct. 1995, pp 491-505.
29. Hah, C. and Loellbach, J., "Development of Hub Corner Stall and its Influence on the Performance of Axial Compressor Blade Rows.,"ASME Paper 97-GT-42, June, 1997.
30. Shabbir, A., Celestina, M.L., Adamczyk, J. J., and Strazisar, A. J., "The Effect of Hub Leakage Flow on Two High Speed Axial Compressor Rotors,"ASME Paper 97-GT-346, June 1997.