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- W3106778129 endingPage "2150043" @default.
- W3106778129 startingPage "2150043" @default.
- W3106778129 abstract "The efficient fuel injection system is a vital part of scramjet for a high-speed flight. In this scientific study, the effects of the multi fuel jets on the inclined surface are investigated at the supersonic air stream with Mach[Formula: see text]. This study employed the CFD technique for the simulation of the interaction of multi hydrogen-jets with free stream airflow. The impressions of inclined surface angle and hydrogen jet total pressure on the fuel mixing zone are disclosed. The Mach contour on the jet plane is presented to describe the chief terms on the distribution and penetration of hydrogen jet inside the combustion chamber. To perform a 3D computational study, the RANS equation with the SST turbulence model is used. Our study shows that the mixing performance of multi jets enhances in high jet pressure when the angle of the tending exterior is raised. Our findings also demonstrate that power and slant of the separation shock is highly effective on the size of the mixing zone." @default.
- W3106778129 created "2020-12-07" @default.
- W3106778129 creator A5037352538 @default.
- W3106778129 creator A5044592175 @default.
- W3106778129 creator A5045155489 @default.
- W3106778129 date "2020-12-24" @default.
- W3106778129 modified "2023-10-12" @default.
- W3106778129 title "Injection of hydrogen sonic multi-jet on inclined surface at supersonic flow" @default.
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- W3106778129 doi "https://doi.org/10.1142/s0129183121500431" @default.
- W3106778129 hasPublicationYear "2020" @default.
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