Combustor Geometry
Combustor Geometry is a structural design specification that defines the physical configuration and dimensional characteristics of the combustion chamber in a scramjet engine, distinguishing it from other propulsion system components by its direct influence on supersonic airflow, fuel mixing efficiency, and thermal management within the context of hypersonic flight.
722
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27.8K
Citations
1.9K
Authors
425
Institutions
Publications per year
2017–2026
323
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722
Akihiro Hayakawa, Yoshiyuki Arakawa, Rentaro Mimoto et al. · International Journal of Hydrogen Energy · 2017 · 370 citations
Engineering, Chemical Engineering, Mechanical Engineering +16
Electric Sail for Spacecraft Propulsion
P. Janhunen · Journal of Propulsion and Power · 2004 · 263 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
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National Institute Of Technology Silchar, India
20 publications · 1.1K citations
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National University of Defense Technology
Changsha, China
32 h-index
190 publications
10K citations

Harbin Institute of Technology
Harbin, China
23 h-index
159 publications
7.5K citations
National Institute Of Technology Silchar
Silchar, India
17 h-index
48 publications
2.8K citations

Hunan University
Changsha, China
17 h-index
52 publications
4.3K citations

Huazhong University of Science and Technology
Wuhan, China
17 h-index
59 publications
2.7K citations
Heilongjiang Institute of Technology
Harbin, China
16 h-index
92 publications
4.7K citations

Beihang University
Beijing, China
16 h-index
68 publications
1.8K citations

Chongqing University
Chongqing, China
15 h-index
94 publications
3.4K citations
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70 publications · 3.7K citations
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AST · 57 publications · 1.9K citations
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39 publications · 1.7K citations
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36 publications · 1.6K citations
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