Supersonic Inlets
Supersonic Inlets is a type of aerodynamic inlet designed to efficiently decelerate and compress supersonic airflow to subsonic speeds for entry into aircraft engines, distinguished by its capability to manage shock waves and maintain stable flow under supersonic flight conditions.
279
Publications
8.8K
Citations
588
Authors
182
Institutions
Publications per year
2017–2026
43
Variants
Supersonic Air Intakes
Parents
279
Experimental Study of Supersonic Inlet Buzz
Simon Trapier, Philippe Duveau, Sébastien Deck · AIAA Journal · 2006 · 151 citations
Engineering, Aerospace Engineering, Mechanical Engineering +14
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588
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182

Glenn Research Center
Cleveland, United States
21 h-index
89 publications
2.3K citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
13 h-index
57 publications
1.5K citations

Sharif University of Technology
Tehran, Iran
12 h-index
31 publications
722 citations
Boeing (Australia)
Brisbane, Australia
9 h-index
18 publications
390 citations

Boeing (United States)
Chicago, United States
9 h-index
19 publications
639 citations
Rutgers, The State University of New Jersey
New Brunswick, United States
6 h-index
20 publications
575 citations
Seoul National University
Seoul, South Korea
6 h-index
14 publications
352 citations

Ames Research Center
Mountain View, United States
6 h-index
10 publications
187 citations
1–8 of 182
30 publications · 1K citations
21
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24 publications · 1.2K citations
18
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AST · 17 publications · 443 citations
15
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18 publications · 584 citations
14
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Repository · 7 publications · 196 citations
7
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1–5