Normal Shock Waves is a discontinuous pressure wave phenomenon in supersonic aerodynamics characterized by an abrupt, near-instantaneous change in fluid properties across a plane perpendicular to the flow direction, distinguishing it from oblique or expansion waves by its orthogonal alignment relative to the upstream velocity vector.
346
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20.9K
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675
Authors
251
Institutions
Publications per year
2017–2026
44
Variants
Normal Shock Wave
Publications
346
1–5 of 346
Authors
675
- HB
14
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1–5 of 675
Institutions
251
University of Cambridge
Cambridge, United Kingdom
16 h-index
44 publications
2.4K citations
Ames Research Center
Mountain View, United States
15 h-index
21 publications
1.9K citations
University of Illinois Urbana-Champaign
Urbana, United States
12 h-index
22 publications
808 citations
Ben-Gurion University of the Negev
Beersheba, Israel
11 h-index
33 publications
867 citations
Langley Research Center
Hampton, United States
9 h-index
12 publications
455 citations
California Institute of Technology
Pasadena, United States
9 h-index
16 publications
2K citations
Stanford University
Stanford, United States
9 h-index
17 publications
2.1K citations
University of Michigan
Ann Arbor, United States
8 h-index
12 publications
274 citations
1–8 of 251
Venues
- Journal of Fluid Mechanics
44 publications · 3.6K citations
28
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- AIAA Journal
38 publications · 5.9K citations
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- Physics of Fluids
29 publications · 1.1K citations
19
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- The Physics of Fluids
20 publications · 1K citations
16
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- Physics of Fluids A Fluid Dynamics
10 publications · 870 citations
10
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