Combined-cycle Propulsion
Combined-Cycle Propulsion is a propulsion system that integrates multiple thermodynamic cycles within a single engine platform to enable efficient operation across a broad speed range by leveraging the distinct performance characteristics of each cycle in its respective flight regime.
178
Publications
5.3K
Citations
481
Authors
144
Institutions
Publications per year
2017–2026
59
Variants
CceCombined-cycle Engine
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481
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144

Northwestern Polytechnical University
Xi'an, China
12 h-index
60 publications
1.9K citations
Japan Aerospace Exploration Agency
Tokyo, Japan
11 h-index
48 publications
1K citations

Glenn Research Center
Cleveland, United States
10 h-index
23 publications
367 citations

Harbin Institute of Technology
Harbin, China
8 h-index
34 publications
1.3K citations

National University of Defense Technology
Changsha, China
8 h-index
30 publications
1.9K citations

Nanjing University of Aeronautics and Astronautics
Nanjing, China
7 h-index
21 publications
547 citations

Beihang University
Beijing, China
5 h-index
18 publications
670 citations

Von Karman Institute for Fluid Dynamics
Sint-Genesius-Rode, Belgium
5 h-index
10 publications
298 citations
1–8 of 144
13 publications · 384 citations
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11 publications · 459 citations
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8 publications · 251 citations
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8 publications · 318 citations
8
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Repository · 6 publications · 127 citations
7
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