Computational Study of Supersonic Flow Past Wall-Mounted Cylindrical Bodies
Author:
Affiliation:
1. Ohio Aerospace Institute
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1433
Reference39 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
2. Shock Wave–Boundary-Layer Interactions
3. Numerical Simulation of Flow over a Submerged Hemispherical Flat-Window Turret
4. Numerical Simulation Exploring Supersonic Flow Over a Forward-Facing Cylindrical Step
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1. Parametric study of supersonic flow over a wall-mounted hemisphere;2018 AIAA Aerospace Sciences Meeting;2018-01-07
2. Investigation of Shock-Boundary Layer Interaction Around Wall-Mounted Hemisphere using DDES and ILES;2018 AIAA Aerospace Sciences Meeting;2018-01-07
3. Automatic Partitioning of Structured Overset Grids for Use with High-Order Algorithms;2018 AIAA Aerospace Sciences Meeting;2018-01-07
4. Investigation of shock wave-boundary-layer interaction for flow over a wall-mounter hemisphere;35th AIAA Applied Aerodynamics Conference;2017-06-02
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