Experimental and numerical investigation of supersonic turbulent flow through a square duct
Author:
Affiliation:
1. University of Washington, Seattle, Washington
2. Informatics General Corporation, NASA Ames Research Center, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9473
Reference28 articles.
1. Survey of viscous interactions associated with high Mach number flight
2. Supersonic interference flow along the corner of intersecting wedges.
3. Supersonic Interaction in the Corner of Intersecting Wedges at High Reynolds Numbers
4. Numerical solutions for supersonic corner flow
5. Three-Dimensional Supersonic Interacting Turbulent Flow along a Corner
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