Comparison of computations using Navier-Stokes equations in rotating and fixed coordinates for flow through turbomachinery
Author:
Affiliation:
1. NSF, Engineering Research Center; Mississippi State Univ., Mississippi State
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-878
Reference13 articles.
1. Research Center under Grant NAG-3-1712, Dr. Eric
2. [I] Choi, D. and Knight C.J."Computations of 3D Viscous Flows in Rotating Turbomachinery Blades,"AIAA-89-0323,Jan. 1989.
3. Ghosh A.R."Solutions to Three-Dimensional Thin-Layer Navier-Stokes Equations in RotatingCoordinatesforFlowthroughTurbomachinery," M.S. Thesis,Mississippi State University, Mississippi,December 1996.
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