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A review of aircraft subsonic and supersonic combustors
Gubran A.Q. Abdulrahman
,
Naef A.A. Qasem
*
,
Binash Imteyaz
,
Ayman M. Abdallah
,
Mohamed A. Habib
*
Corresponding author for this work
Department of Aerospace Engineering
Interdisciplinary Research Center for Sustainable Energy Systems
Department of Mechanical Engineering
Interdisciplinary Research Center for Hydrogen Technologies and Carbon Management
Interdisciplinary Research Center for Aviation and Space Exploration
Research output
:
Contribution to journal
›
Review article
›
peer-review
69
Scopus citations
Overview
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Engineering
Combustor
100%
Combustion
100%
Aircraft
100%
Cavity
83%
Strut
83%
Flame
83%
Flame Stability
66%
Ignition
50%
Supersonic Combustion
50%
Design
50%
Flame Propagation
50%
Engine
33%
Pressure Drop
33%
Thermal Efficiency
16%
Combustion Chamber
16%
Fuel Efficiency
16%
Low Speed
16%
Mixing
16%
Rotating Detonation Engine
16%
Pulse Detonation Engines
16%
High-Speed Aircraft
16%
Research
16%
Fuel
16%
Efficiency
16%
Mixture
16%
High Speed
16%
Physics
Flame Stability
80%
Supersonic Combustion
60%
Flame Holder
60%
Supersonic Combustion Ramjet Engine
40%
Pulse Detonation Engine
20%