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HYDROSTATIC ADJUSTMENT - LAMBS PROBLEM

机译:液压调节-羔羊问题

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The prototype problem of hydrostatic adjustment for large-scale atmospheric motions is presented. When a horizontally infinite layer of compressible fluid, initially at rest, is instantaneously heated, the fluid is no longer in hydrostatic balance since its temperature and pressure in the layer have increased while its density remains unchanged. The subsequent adjustment of the fluid is described in detail for an isothermal base-state atmosphere. The initial imbalance generates acoustic wave fronts with trailing wakes of dispersive acoustic gravity waves. There are two characteristic timescales of the adjustment. The first is the transit time it takes an acoustic front to travel from the source region to a particular location. The second timescale, the acoustic cutoff frequency, is associated with the trailing wake. The characteristic depth scale of the adjustment is the density scale height. If the depth of the heating is small compared with the scale height the final pressure perturbation tends to zero and the pressure field adjusts to the initial density field. For larger depths, there is a mutual adjustment of the pressure and density fields. Use of the one-dimensional analogue of the conservation of Ertel's potential vorticity removes hydrostatic degeneracy and determines the final equilibrium state directly. As a result of the adjustment process, the heated layer has expanded vertically. Since the region below the layer is unaltered, the region aloft is displaced upward uniformly. As a consequence of the expansion, the pressure and temperature anomalies in the layer are reduced from their initial values immediately after the heating. Aloft both the pressure and density fields are increased but there is no change in temperature. Since the base-state atmosphere is isothermal, warm advection is absent; since the vertical displacements of air parcels is uniform aloft, compressional warming is also absent. The energetics of the adjustment are documented. Initially all the perturbation energy resides in the heated layer with a fraction gamma(-1) = 71.4% stored as available potential energy, while the remainder is available elastic energy. A fraction kappa = R/C-p = (gamma - 1)/gamma = 28.6% of the initial energy is lost to propagating acoustic modes. Here gamma = C-p/C-upsilon is the ratio of the specific heats and R is the ideal gas constant. The remainder of the energy is partitioned between the heated layer and the region aloft. The energy aloft appears mostly as elastic energy, and the energy in the layer appears mostly as available potential energy. [References: 18]
机译:提出了用于大范围大气运动的静水压力调节的原型问题。当最初处于静止状态的水平无限的可压缩流体层被瞬间加热时,由于流体在层中的温度和压力增加而密度保持不变,因此流体不再处于静水平衡状态。针对等温基态气氛详细描述了流体的后续调整。初始的不平衡会产生声波前沿,并伴有分散的声重力波的尾波。调整有两个典型的时间尺度。第一个是声波从声源区域到特定位置所花费的传播时间。第二个时标,即声音的截止频率,与尾迹有关。调整的特征深度标度是密度标度高度。如果加热深度小于标尺高度,则最终压力扰动趋于零,并且压力场会调整为初始密度场。对于更大的深度,压力场和密度场会相互调整。使用Ertel潜在涡度守恒的一维类似物可消除静水退化,并直接确定最终的平衡状态。调节过程的结果是,加热层垂直膨胀。由于该层下面的区域保持不变,因此该区域上方的区域均匀向上移动。膨胀的结果是,加热后立即将层中的压力和温度异常从其初始值降低。在高处,压力场和密度场均增加,但温度没有变化。由于基态大气是等温的,因此不存在热对流。由于空气包裹的垂直位移在高处均匀,因此也没有压缩变暖。调整的能量记录在案。最初,所有扰动能量都驻留在加热层中,其中gamma(-1)= 71.4%的分数存储为可用势能,而其余的则是可用弹性能。分数kappa = R / C-p =(gamma-1)/ gamma =初始能量的28.6%被传播的声模损失了。此处,γ= C-p / C-upsilon是比热之比,R是理想气体常数。其余能量在加热层和高空区域之间分配。高处的能量主要表现为弹性能,层中的能量主要表现为可用势能。 [参考:18]

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