Variable Geometry Nozzles
Variable Geometry Nozzles is a specialized type of propulsion nozzle system that belongs to the class of aerospace flow control devices, distinguished by its ability to dynamically alter geometric parameters such as throat area, exit area, or contour in response to varying flight conditions to optimize thrust and engine performance across operational regimes.
53
Publications
1.5K
Citations
180
Authors
74
Institutions
Publications per year
2017–2026
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74

Pennsylvania State University
State College, United States
3 h-index
7 publications
228 citations

Xi'an Jiaotong University
Xi'an, China
2 h-index
7 publications
133 citations

Glenn Research Center
Cleveland, United States
2 h-index
2 publications
77 citations
Japan Aerospace Exploration Agency
Tokyo, Japan
2 h-index
16 publications
336 citations

Langley Research Center
Hampton, United States
2 h-index
3 publications
61 citations
Waseda University
Tokyo, Japan
2 h-index
2 publications
42 citations
Lockheed Martin (United States)
Bethesda, United States
2 h-index
6 publications
75 citations
Bartin University
Bartın, Türkiye
2 h-index
2 publications
132 citations
1–8 of 74
7 publications · 305 citations
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3 publications · 96 citations
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AST · 3 publications · 104 citations
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3 publications · 197 citations
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2 publications · 34 citations
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