A Shock Loss Model for Supersonic Compressor Cascades
Author:
Affiliation:
1. Aero Propulsion and Power Directorate, Wright Laboratory, Wright-Patterson AFB, OH 45433
2. Mechanical Engineering Department, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/121/1/28/5725313/28_1.pdf
Reference33 articles.
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2. Casey, M. V., 1994a, “Computational Methods for Preliminary Design and Geometry Definition in Turbomachinery,” AGARD LS-195, Paper No. 1.
3. Casey, M. V., 1994b, “Industrial Use of CFD in the Design of Turbomachinery,” AGARD LS-195, Paper No. 6.
4. Chima R. V. , 1987, “Explicit Multigrid Algorithm for Quasi-Three-Dimensional Viscous Flows in Turbomachinery,” AIAA Journal of Propulsion and Power, Vol. 3, No. 5, pp. 397–405.
5. Chima, R. V., Turkel, E., and Schaffer, S., 1987, “Comparison of Three Explicit Multigrid Methods for the Euler and Navier–Stokes Equations,” NASA TM-88878.
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