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Fronts in high-temperature laminar gas jets

机译:高温层流气体射流的前沿

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摘要

This paper addresses the slender laminar flow resulting from the discharge of a low-Mach-number hot gas jet of radius a and moderately large Reynolds number Rj into a cold atmosphere of the same gas. We give the boundary-layer solution for plane and round jets with very small values of the ambient-to-jet temperature ratio ε accounting for the temperature dependence of the viscosity and conductivity typical of real gases. It is seen that the leading-order description of the jet in the limit ε → 0 exhibits a front-like structure, including a precisely defined separating boundary at which heat conduction and viscous shear stresses vanish in the first approximation, so that the temperature and axial velocity remain unperturbed outside the jet. Separate analyses are given for the jet discharging into a stagnant atmosphere, when the jet boundary is a conductive front, and for the jet discharging into a coflowing stream, when the jet boundary appears as a contact surface. We provide in particular the numerical description of the jet development region corresponding to axial distances of order Rja for buoyant and non-buoyant jets, as well as the self-similar solutions that emerge both in the near field and in the far field. In all cases considered, comparisons with numerical integrations of the boundary-layer problem for moderately small values of ε indicate that these front descriptions give excellent predictions for the temperature and velocity fields in the near-axis region.
机译:本文讨论了由半径为a的低马赫数热喷流和中等雷诺数Rj的低马赫数热喷流排放到相同气体的冷大气中而产生的细长层流。我们给出了平面和圆形射流的边界层解决方案,其环境与射流温度比ε很小,这说明了真实气体典型的粘度和电导率的温度依赖性。可以看出,在极限ε→0处射流的前导描述呈现出前部状结构,包括精确定义的分隔边界,在该边界处热传导和粘性剪切应力在第一近似中消失。轴向速度在射流外部保持不受干扰。当射流边界为导电前沿时,将对排放到停滞大气中的射流进行单独分析,当射流边界为接触面时,将对排放到同流流中的射流进行单独分析。我们特别提供了对应于浮力和非浮力射流的轴向距离Rja的射流发展区域的数值描述,以及在近场和远场出现的自相似解。在所有考虑的情况下,通过对ε值较小的边界层问题的数值积分进行比较,结果表明,这些正面描述对近轴区域的温度和速度场提供了出色的预测。

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