Mach Number Effects
Mach Number Effects is a theoretical construct in aerodynamics that characterizes the distinct influence of the ratio of flow velocity to the local speed of sound on compressible flow behavior, control surface dynamics, cruise performance, and propulsion efficiency in ramjet engines.
2.7K
Publications
113.4K
Citations
5.4K
Authors
1.2K
Institutions
Publications per year
2017–2026
433
2.7K
1–5 of 2.7K
5.4K
16
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Laboratoire de Mécanique des Fluides et d'Acoustique, France
14 publications · 550 citations
14
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13
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1–5 of 5.4K
1.2K

Langley Research Center
Hampton, United States
40 h-index
264 publications
9.9K citations

Centre National de la Recherche Scientifique
Paris, France
32 h-index
136 publications
5.6K citations

Ames Research Center
Mountain View, United States
27 h-index
78 publications
3.1K citations

Glenn Research Center
Cleveland, United States
26 h-index
95 publications
3K citations
California Institute of Technology
Pasadena, United States
25 h-index
50 publications
3.2K citations
Stanford University
Stanford, United States
23 h-index
68 publications
5.3K citations
University of Cambridge
Cambridge, United Kingdom
23 h-index
50 publications
3.6K citations

Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
22 h-index
62 publications
3.6K citations
1–8 of 1.2K
179 publications · 14.6K citations
62
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232 publications · 11.8K citations
56
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90 publications · 3.2K citations
34
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ApJ · 57 publications · 3.2K citations
32
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65 publications · 3K citations
31
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