The influence of the sinusoidal shock generator on the mixing rate of multi hydrogen jets at supersonic flow
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DOI: 10.1016/j.ast.2019.105579
Abstract: Abstract The rate of fuel mixing inside the combustor is highly significant and effective on the performance of the scramjet engine. In this study, numerical simulations are applied to study the influence of the sinusoidal… read more here.
Keywords: shock generator; sinusoidal shock; rate; influence sinusoidal ... See more keywords
Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber
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DOI: 10.1038/s41598-024-57103-0
Abstract: The importance of the fuel injection configuration on the propulsion efficiency of high-speed vehicles is apparent. In this article, the use of an annular extruded 4-lobe nozzle for the injection of fuel jet in a… read more here.
Keywords: fuel; combustion chamber; fuel mixing; lobe nozzle ... See more keywords
Influence of Finite Width of Shock Generator on Shock-Wave/Boundary-Layer Interaction
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DOI: 10.2514/1.j060076
Abstract: The influence of a finite-width shock generator on the incident shock in the impinging shock-wave/boundary-layer interaction is investigated using different widths of the shock generator. The shock... read more here.
Keywords: influence finite; width shock; shock generator; shock ... See more keywords