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Dynamics of a spherical body shedding from a hypersonic ramp. Part 2. Viscous flow

机译:高超声波坡道球体脱落的动态。 第2.粘性流动

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The separation dynamics of a sphere released from the surface of a ramp into a hypersonic flow is investigated, focusing on the influence of the ramp boundary layer on the sphere behaviour. First, numerical simulations are conducted of a sphere interacting with an isolated high-speed boundary layer to determine the influence on the sphere force coefficients as the sphere diameter and wall-normal location are varied. It is found that the lift coefficient is strongly affected by the near-wall interactions, becoming increasingly negative as the ratio of the sphere radius to boundary-layer thickness, , is decreased. These results are combined with force coefficients derived from simulations of the sphere interacting with the ramp-generated oblique shock to enable numerical predictions of the sphere trajectories for a ramp at Mach 6 (using a similar decoupled approach to Part 1 of this work). It is found that the three trajectory types of the inviscid situation - shock surfing, ejection followed by re-entrainment within the shock layer and direct entrainment - also characterize the sphere behaviour here. Their relative prevalence, however, is influenced by the sphere size: for smaller values of , direct entrainment dominates because of the wall suction, while shock surfing and then ejection/re-entrainment become increasingly likely at larger values of . Increasing the ramp angle and/or the free-stream Mach number reduces the relative influence of the boundary-layer interactions. Finally, experiments are conducted using free-flying spheres released from a ramp surface in a hypersonic shock tunnel, confirming the major trends predicted numerically.
机译:研究了从斜坡表面释放到高超音速流中的球体的分离动力学,重点研究了斜坡边界层对球体行为的影响。首先,对球体与隔离高速边界层的相互作用进行了数值模拟,以确定球体直径和壁面法线位置的变化对球体力系数的影响。研究发现,升力系数受近壁相互作用的强烈影响,随着球体半径与边界层厚度之比的减小,升力系数变得越来越负。这些结果与球体与斜面产生的斜激波相互作用的模拟得出的力系数相结合,以便能够对马赫数为6的斜面的球体轨迹进行数值预测(使用与本工作第1部分类似的解耦方法)。研究发现,无粘情况下的三种弹道类型——激波冲浪、弹射后激波层内的二次夹带和直接夹带——也表征了球体的行为。然而,它们的相对流行率受球体尺寸的影响:对于较小的直径值,由于壁吸力,直接夹带占主导地位,而当直径值较大时,冲击冲浪和弹射/再夹带的可能性越来越大。增加斜坡角和/或自由流马赫数可以减少边界层相互作用的相对影响。最后,在高超音速激波风洞中使用从斜面释放的自由飞行球体进行了实验,证实了数值预测的主要趋势。

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