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Investigation of shock wave-boundary-layer interaction for flow over a wall-mounter hemisphere

Authors :
Miguel R. Visbal
Philip E. Morgan
Scott E. Sherer
Source :
35th AIAA Applied Aerodynamics Conference.
Publication Year :
2017
Publisher :
American Institute of Aeronautics and Astronautics, 2017.

Subjects

Subjects :
Shock wave
020301 aerospace & aeronautics
Boundary layer
0203 mechanical engineering
Flow (mathematics)
Computer science
0103 physical sciences
02 engineering and technology
Mechanics
01 natural sciences
010305 fluids & plasmas

Details

Database :
OpenAIRE
Journal :
35th AIAA Applied Aerodynamics Conference
Accession number :
edsair.doi...........012f5f0d85a7b75c7e9dabc7af0c3c48
Full Text :
https://doi.org/10.2514/6.2017-3403
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