Transonic Boundary Layers
Transonic Boundary Layers is a fluid dynamic phenomenon characterized as a thin viscous region adjacent to a solid surface wherein the flow transitions through Mach numbers near unity, distinguished by the coexistence of subsonic and supersonic regions, strong adverse pressure gradients, and shock wave-boundary layer interactions that critically influence aerodynamic performance and flow separation behavior.
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3.6K
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175
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83
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2017–2026
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Courant Institute of Mathematical Sciences, United States
5 publications · 451 citations
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Ames Research Center
Mountain View, United States
9 h-index
13 publications
483 citations

Langley Research Center
Hampton, United States
7 h-index
13 publications
486 citations

Northwestern Polytechnical University
Xi'an, China
4 h-index
10 publications
498 citations
University of Colorado Boulder
Boulder, United States
3 h-index
6 publications
118 citations
Stanford University
Stanford, United States
3 h-index
3 publications
57 citations
University College London
London, United Kingdom
3 h-index
4 publications
185 citations
University of Michigan
Ann Arbor, United States
3 h-index
5 publications
157 citations
Virginia Tech
Blacksburg, United States
3 h-index
5 publications
119 citations
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19 publications · 533 citations
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7 publications · 456 citations
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Repository · 3 publications · 124 citations
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3 publications · 98 citations
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