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Flux Footprints in the Convective Boundary Layer: Large-Eddy Simulation and Lagrangian Stochastic Modelling

机译:对流边界层的通量足迹:大涡模拟和拉格朗日随机模型

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We investigated the flux footprints of receptors at different heights in the convective boundary layer (CBL). The footprints were derived using a forward Lagrangian stochastic (LS) method coupled with the turbulent fields from a large-eddy simulationmodel. Crosswind-integrated flux footprints shown as a function of upstream distances and sensor heights in the CBL were derived and compared using two LS particle simulation methods: an instantaneous area release and a crosswind linear continuous release. We found that for almost all sensor heights in the CBL, a major positive flux footprint zone was located close to the sensor upstream, while a weak negative footprint zone was located further upstream, with the transition band in non-dimensional upwind distances —X between approximately 1.5 and 2.0. Two-dimensional (2D) flux footprints for a point sensor were also simulated. For a sensor height of 0.158 zi, where zi is the CBL depth, we found that a major positive flux footprint zone followed a weaknegative zone in the upstream direction. Two even weaker positive zones were also present on either side of the footprint axis, where the latter was rotated slightly from the geostrophic wind direction. Using CBL scaling, the 2D footprint result was normalized to show the source areas and was applied to real parameters obtained using aircraft-based measurements. With a mean wind speed in the CBL of U = 5.1 ms~(-1), convective velocity of = 1.37 ms~(-1), CBL depth of zi = 1,000m, and flight track heightof 159 m above the surface, the total flux footprint contribution zone was estimated to range from about 0.1 to 4.5 km upstream, in the case where the wind was perpendicular to the flight track. When the wind was parallel to the flight track, the totalfootprint contribution zone covered approximately 0.5 km on one side and 0.8 km on the other side of the flight track.
机译:我们研究了对流边界层(CBL)中不同高度的受体的通量足迹。足迹是使用正拉格朗日随机(LS)方法与大涡流仿真模型的湍流场相结合得出的。使用两种LS粒子模拟方法,得出并比较了CBL中作为上游距离和传感器高度的函数的侧风积分通量足迹,并进行了比较:瞬时面积释放和侧风线性连续释放。我们发现,对于CBL中几乎所有的传感器高度,主要的正磁通足迹区域位于靠近传感器上游的位置,而弱的负足迹区域位于上游的传感器的上游,过渡带的方向为无量纲的上风向距离-大约1.5和2.0。还对点传感器的二维(2D)通量足迹进行了仿真。对于0.158 zi的传感器高度(其中zi是CBL深度),我们发现在上游方向上主要的正磁通足迹区域紧随弱的负区域。在足迹轴的两侧还存在两个甚至更弱的正区,后者从地转风的方向略微旋转。使用CBL缩放,将二维足迹结果归一化以显示源区域,并将其应用于使用基于飞机的测量获得的真实参数。当CBL中的平均风速为U = 5.1 ms〜(-1),对流速度= 1.37 ms〜(-1),CBL深度zi = 1,000m,飞行轨道高度为地面以上159 m时,在风垂直于飞行轨迹的情况下,总通量足迹贡献区估计在上游约0.1至4.5 km范围内。当风平行于飞行轨迹时,总足迹贡献区在飞行轨迹的一侧大约覆盖0.5 km,在另一侧覆盖0.8 km。

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