Variable Geometry Inlets
Variable Geometry Inlets is a type of airbreathing engine inlet system designed for high-speed propulsion that dynamically adjusts its geometric configuration to optimize airflow compression and pressure recovery across varying flight Mach numbers, particularly in ramjet and scramjet engines.
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2017–2026
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M. Hatami, Michel Cuijpers, Michael D. Boot · Energy Conversion and Management · 2015 · 81 citations · Full text
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University of Manchester
Manchester, United Kingdom
3 h-index
3 publications
83 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
3 h-index
10 publications
320 citations
Tianjin University
Tianjin, China
3 h-index
8 publications
210 citations

Armstrong Flight Research Center
Edwards, United States
2 h-index
2 publications
32 citations

Beihang University
Beijing, China
2 h-index
8 publications
168 citations
University of Michigan
Ann Arbor, United States
1 h-index
3 publications
123 citations

Universidade do Porto
Porto, Portugal
1 h-index
7 publications
455 citations

National University of Ireland
Dublin, Ireland
1 h-index
1 publications
169 citations
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AST · 6 publications · 190 citations
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2 publications · 120 citations
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2 publications · 84 citations
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1 publications · 14 citations
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1 publications · 10 citations
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