Structure of supersonic turbulent flow past a swept compression corner
Author:
Affiliation:
1. Rutgers University, New Brunswick, New Jersey 08903
2. NASA Ames Research Center, Moffett Field, California 94035
3. Princeton University, Princeton, New Jersey 08544
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11006
Reference25 articles.
1. Swept shock/boundary-layer interactions - Tutorial and update
2. A hybrid explicit-implicit numerical algorithm for the three-dimensional compressible Navier-Stokes equations
3. Calculation of three-dimensional shock/turbulent boundary-layer interaction generated by sharp fin
4. Structure of supersonic turbulent flow past a sharp fin
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