Parametric study of supersonic flow over a wall-mounted hemisphere
Author:
Affiliation:
1. Ohio Aerospace Institute
2. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1786
Reference42 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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3. Comparison of Two High-Order Large Eddy Simulation Solvers for Flow Over a Wall-Mounted Hemisphere;AIAA Scitech 2020 Forum;2020-01-05
4. Numerical Simulation of Transonic and Supersonic Flow Over a Wall-Mounted Hemisphere;AIAA Aviation 2019 Forum;2019-06-15
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