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Unsteady Laminar Buoyant Flow Through Rectangular Vents in Large Enclosures

机译:大型外壳中通过矩形通风孔的不稳定层流浮力

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This computational study concentrates on transient laminar flow of air through rectangular vents in horizontal partitions between two large enclosures. For a vent aspect ratio of 1, three flow regimes were identified as the Rayleigh number (Ra) was varied from 1 x 10~3 to 5 x 10~4 based on flow parameters in the vent and corresponding modes of heat transfer through it. The Rayleigh number was found to be the critical control parameter, which determined the flow regimes of conduction, countercurrent, and oscillatory flow regimes. As the effective driving potential decreased with time, flow changed from one regime to the other so that higher-Rayleigh-number results showed all three regimes over time. Circulation patterns within the vent for the conduction regime (Ra < 1500) appeared to follow Chandrasekhar's well-known linear stability results. At higher Ra, sudden bursts of upflow with corresponding downflow have been documented and compared with experimental observations in the literature. The time traces of velocity and temperature fields for this flow regime reveal interesting mechanisms, which have been explained.
机译:这项计算研究的重点是通过两个大围墙之间水平隔板中矩形通风孔的瞬时空气层流。对于通风孔纵横比为1的情况,根据通风孔中的流量参数和通过通风孔的相应传热模式,瑞利数(Ra)从1 x 10〜3变为5 x 10〜4,确定了三种流动方式。发现瑞利数是关键的控制参数,它决定了传导,逆流和振荡流态的流态。随着有效驱动力随时间降低,流量从一种状态变为另一种状态,因此较高的瑞利数结果显示了这三种状态随时间的推移。通风口内的传导方式(Ra <1500)的循环方式似乎遵循钱德拉塞卡(Chandrasekhar)的线性稳定性结果。在较高的Ra下,已经记录了突然的上冲突然爆发和相应的下冲,并将其与文献中的实验观察结果进行了比较。该流态的速度和温度场的时间轨迹揭示了有趣的机理,这些机理已得到解释。

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