Hypersonic Stability
Hypersonic Stability is a theoretical construct in aerodynamic stability analysis that specifically characterizes the tendency of a vehicle or flowfield to maintain or return to a desired trajectory or equilibrium state during atmospheric flight at Mach numbers typically exceeding five, distinguished from subsonic or supersonic stability by the dominant influence of high-temperature gas effects, viscous interactions, and shock wave nonlinearity.
382
Publications
16K
Citations
772
Authors
196
Institutions
Publications per year
2017–2026
115
Parents
382
1–5 of 382
772
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United States Air Force Research Laboratory, United States
12 publications · 872 citations
11
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10
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1–5 of 772
196

Langley Research Center
Hampton, United States
25 h-index
75 publications
3.3K citations
Purdue University West Lafayette
West Lafayette, United States
16 h-index
38 publications
1.7K citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
14 h-index
24 publications
1K citations
Tianjin University
Tianjin, China
13 h-index
36 publications
1.7K citations

Northwestern Polytechnical University
Xi'an, China
12 h-index
28 publications
1.3K citations
University of California, Los Angeles
Los Angeles, United States
12 h-index
26 publications
774 citations

Beihang University
Beijing, China
11 h-index
30 publications
1K citations
University of Maryland, College Park
College Park, United States
11 h-index
24 publications
913 citations
1–8 of 196
31 publications · 1.6K citations
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34 publications · 1.5K citations
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AST · 20 publications · 797 citations
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20 publications · 907 citations
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12 publications · 431 citations
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