Scramjet Transition is the aerodynamic and thermodynamic process by which a ramjet engine operating in subsonic combustion mode transitions to supersonic combustion within the engine flowpath, enabling sustained scramjet operation at hypersonic flight speeds.
70
Publications
3.3K
Citations
187
Authors
55
Institutions
Publications per year
2017–2026
13
Parents
Publications
70
1–5 of 70
Authors
187
- MK
7
h-index
- CP
6
h-index
- RD
5
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- JC
4
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- MG
4
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1–5 of 187
Institutions
55
Langley Research Center
Hampton, United States
12 h-index
25 publications
890 citations
University of Virginia
Charlottesville, United States
7 h-index
23 publications
736 citations
The University of Queensland
Brisbane, Australia
6 h-index
21 publications
911 citations
United States Air Force Research Laboratory
Wright-Patterson AFB, United States
5 h-index
8 publications
406 citations
Northwestern Polytechnical University
Xi'an, China
4 h-index
13 publications
255 citations
Heilongjiang Institute of Technology
Harbin, China
4 h-index
17 publications
475 citations
Harbin Institute of Technology
Harbin, China
4 h-index
17 publications
475 citations
The Ohio State University
Columbus, United States
3 h-index
4 publications
757 citations
1–8 of 55
Venues
- Journal of Propulsion and Power
23 publications · 1.2K citations
20
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- Aerospace Science and Technology
AST · 4 publications · 104 citations
4
h-index
- Journal of Spacecraft and Rockets
3 publications · 59 citations
3
h-index
- NASA STI Repository (National Aeronautics and Space Administration)
Repository · 3 publications · 91 citations
3
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- Acta Astronautica
3 publications · 116 citations
3
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1–5