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Experimental investigation of the effects of heat release on mixing processes and flow structure in a high-speed subsonic turbulent H_2 jet

机译:热释放对高速亚音速湍流H_2射流混合过程和流动结构影响的实验研究

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In this paper, we explore the effects of heat release on mixing and flow structure in a high-speed subsonic turbulent H_2 jet in an air coflow. Heat release effects are determined from the comparison of nonreacting and reacting jet behavior, boundary conditions being identical in both cases. Experiments are performed in a wind tunnel specifically designed for this purpose. Planar laser induced fluorescence on OH radicals and on acetone (seeded in the hydrogen jet) are used to characterize the cartography of scalars, and laser Doppler velocimetry is used to characterize velocity profiles in the far field of the H_2 jet. Results show significant effects of heat release on mixing and flow structure, indicating an overall reduction of mixing and entrainment in the reacting jet compared to the nonreacting jet. First, a change is observed in the orientation of coherent structures originating from Kelvin-Helmholtz type instabilities, and responsible for air entrainment within the jet, which appear "flatter" in the jet flame. Then, the flame length is increased over what would be predicted from the intersection of the mean stoichiometric contour with the centerline of the nonreacting jet. And finally, the longitudinal average velocity decrease along the jet axis is quicker in the nonreacting jet, and nondimensional transverse velocity fluctuations are about half as high in the reacting jet as in the nonreacting jet, indicating a reduction of the turbulence intensity of the flow in this direction in the jet flame.
机译:在本文中,我们探讨了在气流同流中高速亚音速湍流H_2射流中放热对混合和流动结构的影响。通过比较非反应性和反应性射流行为来确定放热效果,两种情况下的边界条件相同。实验是在专门为此目的设计的风洞中进行的。平面激光诱导的OH自由基和丙酮上的荧光(接种在氢射流中)用于表征标量图,激光多普勒测速仪用于表征H_2射流远场中的速度分布。结果表明放热对混合和流动结构有显着影响,表明与非反应射流相比,反应射流中混合和夹带的总体减少。首先,观察到由Kelvin-Helmholtz类型的不稳定性引起的相干结构的方向发生了变化,并引起了喷气机内部的空气夹带,在喷气机火焰中这种空气显得“更平坦”。然后,火焰长度增加到超出平均化学计量轮廓与非反应射流中心线相交所预测的长度。最后,在非反应射流中沿射流轴的纵向平均速度下降更快,反应射流的无量纲横向速度波动大约是非反应射流的一半,这表明流动的湍流强度降低了。这个方向在喷射火焰中。

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