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- W2313644489 abstract "Combustion of different combinations of fuel-air reactions in scramjet combustion chamber are simulated in this paper. The study is done using a developed CFD tool to analyze the Scramjet flow characteristics. For this purpose cavity-stabilized scramjet combustion chamber is implemented and the flow through combustor is simulated. Cavities has become one of the main interest area of the hypersonic propulsion community due to its effect on flame-holding and mixing efficiency. Cavities stabilize the flow and so enhance the supersonic combustion. Coupled Euler and finite rate chemical reaction equations are employed. Two different combinations of fuel-air as Ethylene-Air and Hydrogen-Air are taken into consideration which are two of the most important and efficient fuels to be used in vehicles flying at hypersonic speeds. Reduced chemical reaction models are used for both of the fuels. Seven species and three reactions for Ethylene-Air and seven species and eight reactions for Hydrogen-Air are the models used for the solution of the reactive flow through combustor." @default.
- W2313644489 created "2016-06-24" @default.
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- W2313644489 date "2015-07-23" @default.
- W2313644489 modified "2023-09-25" @default.
- W2313644489 title "Simulations of Ethylene and Hydrogen Combustions in Scramjet Combustor" @default.
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- W2313644489 doi "https://doi.org/10.2514/6.2015-3750" @default.
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