Significance of fluid flow characteristics in the hydrogen-fuelled scramjet combustor using flame stabilisation analysis
Author:
Affiliation:
1. Department of Mechanical Engineering, National Institute of Technology, Hamirpur, India
Publisher
Informa UK Limited
Subject
Mechanical Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/14484846.2019.1601064
Reference23 articles.
1. Comparison of H2, CH4 and H2O for cooling an aerospace plane
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4. Effect of nozzle shape on the performance of high velocity oxygen-fuel thermal spray system
5. Technology Roadmap for Dual-Mode Scramjet Propulsion to Support Space-Access Vision Vehicle Development
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3. Numerical analysis of supersonic combustion of hydrogen flow characteristics in scramjet combustor toward the improvement of combustion efficiency;International Journal of Hydrogen Energy;2022-10
4. Numerical Investigation of the Shock Train in a Scramjet with the Effects of Back-Pressure and Divergent Angles;Numerical and Experimental Studies on Combustion Engines and Vehicles;2020-11-26
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