Energy Separation and Base Pressure in the Wake of a Circular Cylinder
Author:
Affiliation:
1. University of Leicester
2. National Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-3302
Reference16 articles.
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4. Annular Cascade Testing of Turbine Nozzles at High Exit Mach Numbers
5. Carscallen, W.E., and Oosthuizen, P.H., 1989, "The effect of secondary flows on the redistribution of the total temperature field downstream of a stationary turbine cascade," AGARD-CP-469.
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