Variable Geometry Engines
Variable Geometry Engines is a class of air-breathing propulsion systems in which the physical configuration of key engine components, such as inlet ducts, compressor blades, or exhaust nozzles, can be actively adjusted during operation to optimize performance across varying flight conditions and engine regimes.
64
Publications
2.1K
Citations
204
Authors
79
Institutions
Publications per year
2017–2026
14
64
M. Hatami, Michel Cuijpers, Michael D. Boot · Energy Conversion and Management · 2015 · 81 citations · Full text
1–5 of 64
204
4
h-index
4
h-index
3
h-index
Nanjing University of Aeronautics and Astronautics, China
3 publications · 91 citations
3
h-index
3
h-index
1–5 of 204
79
Cranfield University
Cranfield, United Kingdom
4 h-index
7 publications
130 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
4 h-index
21 publications
582 citations
University of Michigan
Ann Arbor, United States
3 h-index
5 publications
425 citations

Moscow Aviation Institute
Moscow, Russia
3 h-index
7 publications
171 citations
Ford Motor Company (United States)
Dearborn, United States
3 h-index
4 publications
490 citations
Universitat Politècnica de València
Valencia, Spain
2 h-index
9 publications
230 citations

Shanghai Jiao Tong University
Shanghai, China
2 h-index
6 publications
122 citations
Technische Universität Braunschweig
Braunschweig, Germany
2 h-index
5 publications
88 citations
1–8 of 79
10 publications · 226 citations
10
h-index
AST · 3 publications · 99 citations
3
h-index
3 publications · 37 citations
3
h-index
3 publications · 72 citations
3
h-index
2 publications · 59 citations
2
h-index
1–5