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Effect of Unmixedness in Large Eddies on Ignition and Combustion of Turbulent Jets of the Fuel in a Supersonic Flow

机译:大涡流中混合气对超音速流动燃料湍流点火和燃烧的影响

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摘要

A method and results of computing the influence of unmixedness in large eddies generated by instability of a contact discontinuity on ignition and combustion of turbulent jets of a fuel in a supersonic flow are presented.The basic system of equations is the Reynolds-averaged Navier-Stokes equations.The influence of unmixedness on chemical reaction rates is reproduced by using a random number generator adjusted in accordance with the probability of origination of favorable conditions for proceeding of chemical reactions,which is computed in each node of the computational grid.The problem of combustion of a plane hydrogen jet injected into a supersonic flow along the plate surface is considered as an example.It is shown that allowance for unmixedness in the case where the flow and the jet have favorable initial parameters for self-ignition leads to a delay in heat release and to origination of pressure and temperature fluctuations.As the parameters approach the self-ignition limit,these fluctuations increase,and the combustion becomes intermittent.
机译:提出了一种计算方法和结果,该方法和结果计算了接触不连续性的不稳定性对超声速流动中燃料湍流燃料的点火和燃烧产生的大涡度的影响。通过使用随机数发生器来再现未混合性对化学反应速率的影响,该发生器根据在化学网格中进行计算的有利条件的发生概率进行调整,该随机数发生器在计算网格的每个节点中进行计算。以沿板表面注入超音速流中的平面氢射流为例进行了研究,结果表明,当射流和射流具有良好的自燃初始参数时,允许混合不均匀会导致热量延迟释放并引起压力和温度波动。随着参数接近自燃极限,这些波动增加,燃烧变得间歇性。

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