Simulation of Hypersonic-Shock-Wave–Laminar-Boundary-Layer Interaction over Blunt Fin

Authors :: Mahsa Mortazavi
Doyle Knight
Source :: AIAA Journal. 57:3506-3523
Publication Year :: 2019
Publisher :: American Institute of Aeronautics and Astronautics (AIAA), 2019.
Abstract: Shock-wave–boundary-layer interaction is one of the most important phenomena in hypersonic flights due to its ubiquitous presence and its extreme effects on the aerothermodynamic loads on the aircr...

Subjects :: Shock wave
020301 aerospace & aeronautics
Hypersonic speed
Materials science
Fin
Hypersonic flight
Aerospace Engineering
Laminar flow
02 engineering and technology
Mechanics
Perfect gas
01 natural sciences
010305 fluids & plasmas
Boundary layer
0203 mechanical engineering
0103 physical sciences
Swept wing

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