Numerical Simulation on Hypersonic Combustion of Hydrogen-Fueled Scramjet Combustor with Parallel Strut Fuel Injection at a Flight Mach Number of 7
2015 ◽
Vol 766-767
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pp. 1044-1049
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Removed due to plagiarism. The original was published as: Numerical Investigation of Inlet-Combustor Interactions for a Scramjet Hydrogen-Fueled Engine at a Flight Mach number of 8. Authors: Edder Rabadan and Bernhard Weigand 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012. Paper ID AIAA-2012-5926, DOI: 10.2514/6.2012-5926
2016 ◽
Vol 9
(3)
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pp. 1215-1220
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2011 ◽
Vol 19
(03)
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pp. 177-183
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2000 ◽
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2016 ◽
Vol 69
(12)
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pp. 1405-1422
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2018 ◽
Vol 176
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pp. 334-348
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