Supersonic Boundary Layers
Supersonic Boundary Layers is a type of boundary-layer flow characterized by the presence of supersonic velocities within the boundary layer, distinguished from subsonic boundary layers by the occurrence of compressibility effects, shock waves, and thermal gradients resulting from high-speed external flow exceeding the speed of sound.
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319
Institutions
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2017–2026
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Science and Technology Corporation (United States), United States
10 publications · 884 citations
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Langley Research Center
Hampton, United States
26 h-index
106 publications
3.8K citations

National University of Defense Technology
Changsha, China
23 h-index
169 publications
4.6K citations
Princeton University
Princeton, United States
20 h-index
73 publications
4.7K citations
California Institute of Technology
Pasadena, United States
15 h-index
41 publications
2.3K citations
Institute of Theoretical and Applied Mechanics
Novosibirsk, Russia
14 h-index
54 publications
1.1K citations

Centre National de la Recherche Scientifique
Paris, France
13 h-index
44 publications
1.7K citations

Ames Research Center
Mountain View, United States
13 h-index
25 publications
2.1K citations
Virginia Tech
Blacksburg, United States
12 h-index
35 publications
850 citations
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127 publications · 6.6K citations
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AST · 13 publications · 256 citations
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