Shock Expansions
Shock Expansions is a theoretical construct in transonic aerodynamics that characterizes the interaction and propagation of discontinuous pressure waves and expansion fans in supersonic flow fields, distinguishing itself by describing the nonlinear coupling between shock waves and rarefaction regions during transonic flow evolution.
72
Publications
2.8K
Citations
167
Authors
109
Institutions
Publications per year
2017–2026
8
Parents
72
1–5 of 72
167
4
h-index
3
h-index
Applied Science Laboratories (United States), United States
4 publications · 115 citations
3
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2
h-index
2 publications · 94 citations
2
h-index
1–5 of 167
109

Centre National de la Recherche Scientifique
Paris, France
5 h-index
8 publications
264 citations

Langley Research Center
Hampton, United States
4 h-index
9 publications
210 citations
Commissariat à l'Énergie Atomique et aux Énergies Alternatives
Paris, France
3 h-index
6 publications
610 citations
Applied Science Laboratories (United States)
Bedford, United States
3 h-index
7 publications
105 citations
University of California, Berkeley
Berkeley, United States
3 h-index
3 publications
157 citations

Imperial College London
London, United Kingdom
3 h-index
7 publications
179 citations

Rice University
Houston, United States
2 h-index
3 publications
256 citations
University of California, Los Angeles
Los Angeles, United States
2 h-index
4 publications
884 citations
1–8 of 109
7 publications · 162 citations
7
h-index
5 publications · 154 citations
5
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MCOM · 3 publications · 506 citations
3
h-index
ApJ · 3 publications · 276 citations
3
h-index
2 publications · 124 citations
2
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1–5