Thrust Vectoring Nozzles
Thrust Vectoring Nozzle is a type of propulsion nozzle that mechanically alters the direction of thrust output by deflecting the exhaust jet, thereby enabling controlled maneuverability of aerospace vehicles without relying solely on aerodynamic control surfaces.
85
Publications
2.5K
Citations
166
Authors
59
Institutions
Publications per year
2017–2026
13
Variants
Thrust Vectoring Nozzle
Parents
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59

Langley Research Center
Hampton, United States
20 h-index
43 publications
1.8K citations
Politecnico di Torino
Turin, Italy
5 h-index
10 publications
286 citations

Whitney Museum of American Art
New York, United States
5 h-index
8 publications
210 citations
Pratt & Whitney (United States)
East Hartford, United States
5 h-index
8 publications
210 citations
Gyeongguk National University
Andong, South Korea
4 h-index
10 publications
369 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
4 h-index
16 publications
569 citations

Northwestern Polytechnical University
Xi'an, China
3 h-index
10 publications
154 citations

Armstrong Flight Research Center
Edwards, United States
3 h-index
3 publications
50 citations
1–8 of 59
Repository · 10 publications · 315 citations
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Repository · 9 publications · 160 citations
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5 publications · 214 citations
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4 publications · 73 citations
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4 publications · 61 citations
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