Impact of CFD on test and evaluation at the Compressor Research Facility
Author:
Affiliation:
1. USAF, Wright Lab., Wright-Patterson AFB, OH
2. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2881
Reference24 articles.
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2. Three-Dimensional Flow Phenomena in a Transonic, High-Throughflow, Axial-Flow Compressor Stage
3. 4Chen, Y. S., 1988, "3-D Stator-Rotor Interaction of the SSME," AIAA Paper No. 88-3095.
4. 5Giles, M. B., 1988,"Stator/Rotor Interaction in a Transonic Turbine,"AIAA Paper No. 88-3093.
5. 6Jorgenson, P. C. E. and Chima, R. V., 1988,"An Explicit Runge-Kutta Method for Unsteady Rotor/Stator Interaction,"AIAA PaperNo. 88-0049.
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1. Numerical Simulation of the Shock-Tip Leakage Vortex Interaction in a HPC Front Stage;Journal of Turbomachinery;1999-07-01
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