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Dynamics of laboratory simulated microbursts.

机译:实验室模拟微爆的动力学。

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A downburst (or microburst) is an intense, localized downdraft of cold air which reaches the Earth and spreads radially outward after it impinges on the ground. Downdrafts are typically induced by rapid evaporation of moisture or melting of hail. The divergent outflow created by a microburst produces strong winds in opposite directions. The sudden changes in the speed and direction of both horizontal and vertical winds within a microburst can create hazardous conditions for aircraft within 1000 ft of the ground, particularly during takeoff and landing. The objective of this investigation was to obtain detailed measurements within a laboratory-simulated version of this flow.; The flow was modeled experimentally by releasing a small volume of heavier fluid into a less dense ambient surrounding. The heavier fluid impinged on a horizontal plate which represented the ground. Indices of refraction of the light and heavy fluid were matched to yield clear photographic images. Particle image velocimetry (PIV) was used to obtain detailed maps of the instantaneous velocity fields within horizontal and vertical cross sections through the flow. Laser-induced fluorescence (LIF) was used to determine the local concentration of heavy fluid within the downburst flow at different times.; PIV measurements showed that the leading edge of the falling fluid rolled up into a vortex ring which then impacted on the ground and expanded radially outward. After touchdown, the largest horizontal velocities occurred beneath the vortex ring but also extended over some distance upstream of the vortex core. PIV results showed small vertical velocity gradients in the region below the core of the vortex ring. The effects of parameters such as initial release height and release volume shape were investigated.; Using appropriate length and time scales, the measured velocities were scaled to and compared with previously studied atmospheric microbursts. The experimental data generally agree well with observed and numerically simulated data. Also, the scaled velocity fields were used to construct sequences of events that an aircraft might encounter while traversing a microburst at low altitudes.
机译:突发性爆发(或微爆发)是一种强烈的局部向下的冷空气流,它到达地球并在撞击地面后沿径向向外扩散。下降气流通常是由水分的快速蒸发或冰雹融化引起的。微爆产生的发散流出会产生相反方向的强风。在微暴中水平和垂直风的速度和方向的突然变化会给距地面1000英尺以内的飞机造成危险,特别是在起飞和着陆期间。该调查的目的是在该流程的实验室模拟版本中获得详细的测量结果。通过将少量较重的流体释放到密度较小的周围环境中,对流动进行了实验建模。较重的流体撞击在代表地面的水平板上。使轻和重流体的折射指数相匹配以产生清晰的摄影图像。粒子图像测速仪(PIV)用于获得通过水流的水平和垂直截面内的瞬时速度场的详细地图。激光诱导荧光(LIF)用于确定不同时间下突流内重液的局部浓度。 PIV测量显示,下落的流体的前缘卷成一个涡流环,然后撞击到地面并径向向外扩展。着陆后,最大水平速度出现在涡流环下方,但也延伸到涡流核上游一定距离。 PIV结果表明,在涡环核心下方的区域中,垂直速度梯度较小。研究了初始释放高度和释放体积形状等参数的影响。使用适当的长度和时间标度,将测得的速度定标为与先前研究的大气微暴并比较。实验数据通常与观察到的数值模拟数据非常吻合。同样,缩放后的速度场用于构造飞机在低空穿越微爆时可能遇到的事件序列。

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