Comparison of the AUSM+ and H-CUSP Schemes for Turbomachinery Applications-Reference-Cited by-同舟云学术

Comparison of the AUSM+ and H-CUSP Schemes for Turbomachinery Applications

Published:2003-06-23 Issue: Volume: Page:
ISSN:
Container-title:16th AIAA Computational Fluid Dynamics Conference
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Author:

Chima Rodrick¹,Liou Meng-Sing¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4120

Reference30 articles.

1. Dunham, J., ed. "CFD Validation for Propulsion System 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,June1998.

3. Reid,L.,andMoore,R.D."DesignandOverallPerformance of Four Highly-Loaded, High-Speed Inlet Stages for an Advanced, High-Pressure-Ratio Core Compressor,"NASATP-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. 5Tweedt,D.L.,Chima,R.V.,andTurkel,E."PreconditioningforNumericalSimulationofLowMachNumber Three-Dimensional Viscous Turbomachinery Flows," AIAAPaper97-1828,June,1997.

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