首页> 外文期刊>International Journal of Heat and Mass Transfer >Vortex Formation And Heat Transfer In Turbulent Flow Past A Transverse Cavity With Inclined Frontal And Rear Walls
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Vortex Formation And Heat Transfer In Turbulent Flow Past A Transverse Cavity With Inclined Frontal And Rear Walls

机译:前壁和后壁倾斜的横向腔经过湍流时的涡流形成和传热

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The process of vortex formation, distributions of pressure coefficients, and convective heat transfer in a turbulent flow past a cavity with a low aspect ratio and inclined frontal and rear walls were experimentally studied. The angle of wall inclination φ was varied in the interval from 30° to 90°. Visualization techniques were applied to trace the evolution of the flow with the angle φ as the transverse cavity became more open. Pressure fields in the longitudinal and transverse sections on the bottom wall of the cavity, and on its frontal and rear walls, were measured. The measured distributions of temperature in the longitudinal and transverse sections on the three heated walls, and the obtained thermographic fields over the whole heated surface, were used to calculate local and average heat-transfer coefficients. It is found that in the interval of wall inclination angles φ = 60-70° the flow in the cavity becomes unstable, with the primary vortex changing its structure from single-cellular to double-cellular. As a result, the distributions of static pressure and surface temperature across and along the cavity suffer dramatic changes. At smallest angles φ the flow re-attachment point gets displaced into the cavity to cause an abrupt growth of pressure and heat-transfer coefficients on the rear wall, which leads to a slight increase of the surface-mean pressure and heat transfer inside the cavity. At the angle of instability, φ = 60°, the local heat-transfer coefficient decreases markedly over the cavity span from the end faces of the cavity toward its center, and a most pronounced intensification of heat transfer is observed.
机译:实验研究了湍流通过低长径比,前后壁倾斜的湍流中的涡流形成,压力系数分布和对流传热的过程。壁倾角φ在30°到90°之间变化。应用了可视化技术来追踪随着横向腔变得更加开放的角度为φ的流体的演化。测量空腔底壁以及其前后壁的纵向和横向截面中​​的压力场。在三个加热壁的纵向和横向截面上测得的温度分布,以及在整个加热表面上获得的热成像场,用于计算局部和平均传热系数。结果发现,在壁倾角φ= 60-70°的区间内,腔中的流动变得不稳定,主旋涡将其结构从单细胞改变为双细胞。结果,整个空腔内和沿着空腔的静压和表面温度的分布都发生了急剧的变化。在最小角度φ处,流重新连接点移入空腔,导致后壁上的压力和传热系数突然增长,这导致空腔内的表面平均压力和传热略有增加。在不稳定性角φ= 60°时,从腔的端面到腔的中心,腔的整个传热系数在腔的跨度上明显降低,并且观察到最明显的传热增强。

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