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Numerical simulations of high frequency transverse pulsed jet injection into a supersonic crossflow

机译:高频横向脉冲喷射注入超声波横流的数值模拟

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The design of scramjet engines includes the investigation of minimally intrusive fuel delivery mechanisms which maximize jet fuel penetration and mixing. In subsonic crossflows it has been shown that pulsation of gaseous jets can improve jet penetration and mixing in comparison to unforced (steady) jets. Extensive investigations have already explored subsonic flow regimes for pulsed injection; however, only a limited number of experimental and numerical studies have been performed which investigate pulsed jets in a supersonic crossflow. This study presents fully three-dimensional (3D) scale-resolving simulations of steady and a sinusoidally pulsed jet (f = 16 kHz) using a wall modeled large eddy simulation approach to capture large-scale vortical structures in turbulent jet in supersonic crossflow and pulsed jet in supersonic crossflow. A block-structured, fully 3D turbulent scale resolving finite volume model was used to explore physics simulations of steady and pulsed jets in a supersonic crossflow. The results of the simulations presented show that sinusoidal pulsation of a gaseous hydrogen jet improves penetration and mixing over the steady jet when the momentum flux ratios are equivalent. (C) 2020 Elsevier Masson SAS. All rights reserved.
机译:Scramjet发动机的设计包括对最大限度地提高喷射燃料渗透和混合的最小侵入式燃料输送机构的研究。在亚源交叉流中,已经表明,与未粘的(稳定的)喷射相比,气体喷射的脉动可以改善喷射渗透和混合。广泛的调查已经探讨了脉冲注射的亚音流状态;然而,已经仅进行了有限数量的实验和数值研究,该研究在超声波横流中调查了脉冲喷射。本研究呈现了使用墙体建模的大型涡流模拟方法的稳定和正弦脉冲射流(F = 16 kHz)的三维(3D)尺度分辨模拟,以捕获超声波横流和脉冲中的湍流喷射中的大规模涡流结构在超音速交叉流动的喷气机。一种块结构的完全3D湍流尺度解析有限体型模型用于探索超声波横流中稳定和脉冲喷射的物理模拟。提出的模拟结果表明,当动量助焊剂比率等同时,气态氢气喷射的正弦脉动改善了稳定喷射的穿透和混合。 (c)2020 Elsevier Masson SAS。版权所有。

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