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Recent advances in cavity-based scramjet engine- a brief review
International Journal of Hydrogen Energy, 2019At present, the critical issue related to design of scramjet engine is to achieve efficient mixing between the air and fuel. Among the several fuel injection strategies, cavity flame holder is identified as a well-organized method for supporting the ...
Kulmani Mehar, K M Pandey, Wei Huang
exaly +2 more sources
Hydrogen fuel in scramjet engines - A brief review
International Journal of Hydrogen Energy, 2020Due to the wide flammability range and low ignition delay of Hydrogen, it can burn rapidly and generate a large amount of thrust. It is for this reason alone that many researchers have promoted hydrogen as a potential fuel in scramjet engines.
K M Pandey, Wei Huang, Gautam Choubey
exaly +2 more sources
A brief review on the recent advancement in the field of jet engine - scramjet engine
Materials Today: Proceedings, 2021SCRAMJET engine has become one of the most recent advancement in the field of air breathing hypersonic flight. This paper gives a brief review on recent developments of scramjet combustor and fuels used in scramjet engine.
K M Pandey
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Flame propagation and stabilization in dual-mode scramjet combustors: A survey
Progress in Aerospace Sciences, 2018The dual-mode scramjet combustor is a promising candidate for the combined cycle engine of the hypersonic airplane, and the flame propagation and stabilization process in the dual-mode scramjet combustor has a great impact on its performance improvement.
Rasoul Moradi, Wei Huang, Zhao-Bo Du
exaly +2 more sources
Prospects for scramjet engines in reusable launch applications: A review
International Journal of Hydrogen Energy, 2023Vinod Narayanan +2 more
exaly +2 more sources
Aerospace Science and Technology, 2020
Scramjet is the optimal propulsion system for hypersonic vehicles, and it is important to study its maximum flight Mach number. Upper limit and its influence factors of the flight Mach number of dual-mode scramjet used in hypersonic vehicles are ...
Wen Bao, Kunlin Cheng, Jingfeng Tang
exaly +2 more sources
Scramjet is the optimal propulsion system for hypersonic vehicles, and it is important to study its maximum flight Mach number. Upper limit and its influence factors of the flight Mach number of dual-mode scramjet used in hypersonic vehicles are ...
Wen Bao, Kunlin Cheng, Jingfeng Tang
exaly +2 more sources
The Physics of Fluids, 2023
Scramjet is considered as the future of high-speed transportation and reusable launch vehicle for satellite placement. However, the combustion of fuel at supersonic speeds is a challenge.
Prasanth P. Nair +2 more
semanticscholar +1 more source
Scramjet is considered as the future of high-speed transportation and reusable launch vehicle for satellite placement. However, the combustion of fuel at supersonic speeds is a challenge.
Prasanth P. Nair +2 more
semanticscholar +1 more source
Dual-path flow field reconstruction for a scramjet combustor based on deep learning
The Physics of Fluids, 2022A flow field reconstruction algorithm based on deep learning is an effective method to detect the evolution of wave structure in a scramjet combustor, which is of great significance for accurately predicting the operating performance of the scramjet ...
Xue Deng +5 more
semanticscholar +1 more source
Journal of Fluid Mechanics, 2021
This study investigates the interactions between combustor and isolator and the role played by combustion on choking-induced unstart. Shock train unsteadiness and pressure fluctuations in non-reacting environments have been previously explained in terms ...
D. Baccarella +4 more
semanticscholar +1 more source
This study investigates the interactions between combustor and isolator and the role played by combustion on choking-induced unstart. Shock train unsteadiness and pressure fluctuations in non-reacting environments have been previously explained in terms ...
D. Baccarella +4 more
semanticscholar +1 more source

