Hypersonic Testing
Hypersonic Testing is a type of aerodynamic testing that involves the experimental evaluation of flow characteristics and vehicle performance at speeds exceeding Mach 5, where high-temperature effects, real gas dynamics, and shock wave interactions dominate the flow regime.
1K
Publications
33K
Citations
2.1K
Authors
409
Institutions
Publications per year
2017–2026
165
Parents
1K
1–5 of 1K
2.1K
United States Air Force Research Laboratory, United States
32 publications · 1.3K citations
23
h-index
20
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14
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14
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Calspan-University of Buffalo Research Center, United States
19 publications · 612 citations
14
h-index
1–5 of 2.1K
409

Langley Research Center
Hampton, United States
40 h-index
427 publications
15.4K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
32 h-index
126 publications
5.5K citations
Purdue University West Lafayette
West Lafayette, United States
23 h-index
84 publications
3.7K citations
Deutsches Zentrum für Luft- und Raumfahrt e. V. (DLR)
Cologne, Germany
21 h-index
112 publications
3.4K citations

Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
21 h-index
60 publications
2.8K citations

Ames Research Center
Mountain View, United States
21 h-index
69 publications
2K citations
Sandia National Laboratories
Albuquerque, United States
18 h-index
71 publications
2.6K citations

Armstrong Flight Research Center
Edwards, United States
16 h-index
31 publications
1.2K citations
1–8 of 409
80 publications · 3.1K citations
33
h-index
93 publications · 3.1K citations
32
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27 publications · 1.2K citations
19
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20 publications · 980 citations
18
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AST · 21 publications · 812 citations
17
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