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Mixing Enhancement from Severely Overexpanded Nozzles

机译:严重过度膨胀的喷嘴引起的混合增强

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摘要

Flow exiting a convergent-divergent nozzle operated at severely overexpanded conditions, such that a shock wave is formed inside the nozzle, exhibits a strong instability that causes mixing enhancement in the flow itself and can destabilize an adjacent flow. The latter property enables mixing enhancement of an arbitrary jet via axial injection of a secondary gas flow. A systematic investigation of this phenomenon reveals that the instability is associated with shock-induced nozzle flow separation. In this paper we review key results that demonstrate the potential of this mixing technique and provide insight into the relevant physical processes. In addition, we establish criteria for the occurrence and location of the separation shock, and construct correlations between mixing enhancement and shock strength.
机译:离开会聚-发散喷嘴的流体在严重过度膨胀的条件下运行,从而在喷嘴内部形成冲击波,流动表现出很强的不稳定性,从而导致流体本身的混合增强并可能使相邻流体不稳定。后一特性使得能够通过轴向注入二次气流来增强任意射流的混合。对这种现象的系统研究表明,这种不稳定性与冲击引起的喷嘴流分离有关。在本文中,我们回顾了关键结果,这些结果证明了这种混合技术的潜力,并提供了对相关物理过程的深入了解。此外,我们建立了分离冲击的发生和位置的标准,并构造了混合增强和冲击强度之间的相关性。

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  • 来源
    《International journal of aerospace innovations》 |2010年第4期|p.235-252|共18页
  • 作者单位

    University of California, Irvine, Irvine, CA, 92697-3975 Department of Mechanical and Aerospace Engineering, 4200 Engineering Gateway, Irvine, CA, 92697-3975;

    University of California, Irvine, Irvine, CA, 92697-3975 Department of Mechanical and Aerospace Engineering, 4200 Engineering Gateway, Irvine, CA, 92697-3975;

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  • 入库时间 2022-08-17 23:48:34

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