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Numerical simulation of strongly stratified flow over a three-dimensional hill

机译:三维丘上强分层流的数值模拟

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A numerical study of stably stratified flow over a three-dimensional hill is presented. Large-eddy simulation is used here to examine in detail the laboratory experimental flows described in the landmark work of Hunt and Snyder about stratified flowover a hill. The flow is linearly stratified and U infinity/Nh is varied from 0.2 to 1.0. Here N and U propor. to are the buoyancy frequency and freestream velocity respectively, and h is the height of the hill. The Reynolds number based on the hill height is varied from 365 to 2968. The characteristic flow patterns at various values of U infinity/Nh have been obtained and they are in good agreement with earlier theoretical and experimental results. It is shown that the flow field cannot be predicted by Drazin's theory when recirculation exists at the leeside of the hill even at U infinity/Nh 1. The wake structure agrees well with a twodimensional wake assumption when U infinity/Nh 1 but lee waves start to influence the wake structure as U infinity/Nh increases. The dividing-streamline heights obtained in the simulation are in accordance with experimental results and Sheppard's formula. The energy loss along the dividing streamline due to friction/turbulence approximately offsets the energy gained from pressure field. When lee waves are present, linear theory always underestimates the amplitude and overestimates the wavelength of three-dimensional lee waves. The simulated variations of drag coefficients with the parameter K (= ND/pi U infinity) are qualitatively consistent with experimental data and linear theory. Here D is the depth of the tank.
机译:提出了三维山丘上稳定分层流的数值研究。这里使用大涡模拟来详细检查在Hunt和Snyder的地标性工作中描述的关于分层流过小山的实验室实验流程。流动被线性分层,并且U infinity / Nh从0.2到1.0变化。这里是N和U的propor。分别是浮力频率和自由流速度,h是山的高度。基于山高的雷诺数在365和2968之间变化。已经获得了在U无穷大/ Nh的各种值下的特征流型,并且与早期的理论和实验结果非常吻合。结果表明,即使在U infinity / Nh 1时,在山的后侧存在回流时,流场也无法用Drazin的理论进行预测。当U infinity / Nh 1时,尾流结构与二维尾流假设吻合良好但是随着U无穷大/ Nh的增加,回风开始影响尾波的结构。在模拟中获得的分流线高度符合实验结果和Sheppard公式。由于摩擦/湍流,沿着分流线的能量损失大约抵消了从压力场获得的能量。当存在回风时,线性理论总是低估了振幅,而高估了三维回风的波长。参数为K(= ND / pi U无穷大)的阻力系数的模拟变化在质量上与实验数据和线性理论一致。 D是水箱的深度。

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