Supersonic Combustion is a combustion process in which fuel reacts with oxidizer within a supersonic airflow, distinguished from subsonic combustion by maintaining flow velocities above Mach 1 throughout the reaction zone, enabling efficient propulsion in hypersonic scramjet engines.
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Research on supersonic combustion
F. S. Billig · Journal of Propulsion and Power · 1993 · 443 citations
Engineering, Aerospace Engineering, Mechanical Engineering +14
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466
National University of Defense Technology
Changsha, China
39 h-index
389 publications
18.9K citations
Langley Research Center
Hampton, United States
35 h-index
173 publications
6.9K citations
United States Air Force Research Laboratory
Wright-Patterson AFB, United States
27 h-index
85 publications
6.3K citations
The University of Queensland
Brisbane, Australia
25 h-index
88 publications
3.6K citations
Chinese Academy of Sciences
Beijing, China
24 h-index
119 publications
4.6K citations
Wright-Patterson Air Force Base
Wright-Patterson AFB, United States
22 h-index
44 publications
5.5K citations
Stanford University
Stanford, United States
21 h-index
80 publications
6K citations
Northwestern Polytechnical University
Xi'an, China
20 h-index
132 publications
4.3K citations
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Venues
- Journal of Propulsion and Power
151 publications · 9.8K citations
54
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- AIAA Journal
82 publications · 4.5K citations
35
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- Combustion and Flame
41 publications · 2.6K citations
33
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- International Journal of Hydrogen Energy
49 publications · 3K citations
32
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- Acta Astronautica
51 publications · 1.9K citations
25
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