Variable-cycle Hypersonic Engines
Variable-Cycle Hypersonic Engines is a type of air-breathing propulsion system that integrates multiple thermodynamic cycles within a single engine architecture to enable efficient and stable operation across a wide range of flight Mach numbers, particularly transitioning seamlessly from supersonic to hypersonic speeds by adaptively modulating airflow pathways and combustion modes.
11
Publications
405
Citations
24
Authors
14
Institutions
Publications per year
2017–2026
1
Variants
Variable Cycle Hypersonic Engines
Parents
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Glenn Research Center
Cleveland, United States
2 h-index
2 publications
99 citations
General Electric (United States)
Boston, United States
2 h-index
2 publications
109 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
1 h-index
2 publications
28 citations
General Electric (Sweden)
Uppsala, Sweden
1 h-index
1 publications
85 citations
Tianjin Tanggu Women and Child Health
Tianjin, China
1 h-index
1 publications
11 citations

Beihang University
Beijing, China
1 h-index
5 publications
215 citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
1 h-index
1 publications
78 citations
Georgia Institute of Technology
Atlanta, United States
1 h-index
5 publications
105 citations
1–8 of 14
Repository · 1 publications · 66 citations
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Conference · 1 publications · 14 citations
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Conference · 1 publications · 21 citations
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1 publications · 78 citations
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1 publications · 43 citations
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