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Numerical Analyses of Wave Generation and Vortex Formation under the Action of Viscous Fluid Flows over a Depression

机译:凹陷上粘性流体作用下波浪产生和涡旋形成的数值分析。

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Transient free-surface deformations and evolving vortices due to the passage of flows over a submerged cavity are simulated. A two-dimensional stream function–vorticity formulation with a free-surface model is employed. Model results are validated against the limiting case of pure lid-driven cavity flow with comparisons of the vortical flow pattern and velocity profiles. The verification of the free-surface computations are also carried out by comparing results with published potential flow solutions for cases of flows over a depressed bottom topography. The agreements are generally good. Investigations are extended to other viscous flow conditions, where the cavity is set to have the normalized dimension of one by one when scaled by the still water depth. The free-surface elevations and streamline patterns for cases with Froude numbers ranging from 0.5 to 1.1 and different Reynolds numbers ( Re = 5000 and 500) are calculated. At the condition of near-critical flow ( Fr ≈ 1.0), the phenomenon of upstream advancing solitons is produced. Viscous effects on the free-surface profile reveal that at a lower value of Re (e.g., Re = 500) larger advancing solitary waves are generated. Vortical flow patterns in the cavity are examined for the cases with Fr = 1.0 and various values of Re . When Re = 5000, the vortex pattern includes a primary and a weak, but dominated secondary vortices at the time reaching a nearly quasi-steady motion. For the case of lower Re (e.g., Re = 500), a steady-state vortex pattern can be established with a clockwise primary vortex mostly occupied inside the cavity.
机译:模拟了由于流过淹没腔而造成的瞬态自由表面变形和涡旋。采用具有自由表面模型的二维流函数-涡度公式。通过对涡旋流型和速度分布图的比较,对纯盖驱动腔流的极限情况验证了模型结果。通过将结果与公布的潜在水流解决方案进行比较,也可以对自由表面计算进行验证,以解决凹陷底部地形上的水流情况。协议通常是好的。研究范围扩展到其他粘性流动条件,其中将空腔设置为当按静止水深缩放时,归一化尺寸为一一。计算Froude数在0.5到1.1之间且雷诺数不同(Re = 5000和500)的情况下的自由表面高程和流线型态。在接近临界流动(Fr≈1.0)的条件下,会产生上游推进孤子现象。对自由表面轮廓的粘性影响表明,在较低的Re值(例如Re = 500)下,会产生较大的行进孤立波。对于Fr = 1.0和Re的各种值的情况,检验了空腔中的涡流模式。当Re = 5000时,涡旋图样在达到近似准稳态运动时包括一个主旋涡和一个微弱但占优势的次旋涡。对于较低的Re(例如Re = 500),可以建立一个稳态的涡流模式,其中顺时针的主要涡流主要占据腔体内。

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