Prandtl-meyer Flow
Prandtl-Meyer Flow is a theoretical model in supersonic aerodynamics that describes the isentropic expansion of a supersonic flow around a convex corner, characterized by a continuous fan of expansion waves that increase the flow Mach number while decreasing pressure and density.
42
Publications
1.7K
Citations
73
Authors
48
Institutions
Publications per year
2017–2026
4
Parents
42
A Fundamental Derivative in Gasdynamics
P. A. Thompson · The Physics of Fluids · 1971 · 344 citations
Equations, tables, and charts for compressible flow
nasa · 2019 · 278 citations
The perturbed region behind a diffracting shock wave
B. W. Skews · Journal of Fluid Mechanics · 1967 · 140 citations
1–5 of 42
73
United States Air Force Research Laboratory, United States
2 publications · 146 citations
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1–5 of 73
48
Princeton University
Princeton, United States
3 h-index
6 publications
245 citations

University of Blida
Blida, Algeria
2 h-index
3 publications
63 citations
University of Michigan
Ann Arbor, United States
2 h-index
3 publications
51 citations
University of Wisconsin–Madison
Madison, United States
2 h-index
2 publications
33 citations

University of Manchester
Manchester, United Kingdom
2 h-index
2 publications
34 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
2 h-index
6 publications
458 citations
University of Oxford
Oxford, United Kingdom
2 h-index
2 publications
33 citations
Pohang University of Science and Technology
Pohang, South Korea
2 h-index
2 publications
33 citations
1–8 of 48
9 publications · 193 citations
9
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5 publications · 205 citations
5
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5 publications · 403 citations
5
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2 publications · 78 citations
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Conference · 2 publications · 146 citations
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1–5