首页> 外文期刊>Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics >Influence of the velocity distribution at the inlet boundary on the CFD prediction of local velocity and pressure fields around a hydrofoil
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Influence of the velocity distribution at the inlet boundary on the CFD prediction of local velocity and pressure fields around a hydrofoil

机译:入口边界处的速度分布对水翼周围局部速度和压力场的CFD预测的影响

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摘要

A study of the influence of the inlet boundary condition on simulation results is presented. Experimental measurements and simulations of the flow over a hydrofoil in a closed circuit cavitation tunnel were performed. Using the LDA method the velocity profile, 365 mm upstream of the hydrofoil, was measured. PIV method combined with the LIF technique was used for the determination of the velocity field in the vicinity of the hydrofoil. Static pressure at 38 positions on the surface of the hydrofoil was measured. The CFD code Fluent was used for the simulations. A RANS approach with the k-epsilon RNG turbulence model was applied. Two simulations of the fluid flow were performed - one with a uniform (ideal) velocity profile at the inlet of the computational domain and the other with the experimentally deter-mined velocity profile. The simulation with the ideal boundary condition produced rather poor results with a considerable discrepancy to the experimental measurements. On the other hand the simulation produced more accurate results when the real (measured) boundary condition was used. The influence of the boundary condition could be seen in x- and y-velocity component in the vicinity of the hydrofoil, in c(p) distribution on the surface of the hydrofoil and in the evolution of the velocity profiles downstream of the inlet. It was concluded that it is essential to either use the real (measured) velocity profiles for the inlet boundary condition or to assure that the real upstream flow is almost ideally uniform, if an accurate simulation result is required. (C) 2007 Elsevier Inc. All rights reserved.
机译:研究了入口边界条件对仿真结果的影响。进行了闭环空化隧道中水翼上流动的实验测量和模拟。使用LDA方法,测量了水翼上游365毫米的速度分布。 PIV方法结合LIF技术用于确定水翼附近的速度场。测量了水翼表面38个位置的静压力。 CFD代码Fluent用于仿真。应用了带有K-εRNG湍流模型的RANS方法。进行了两种流体流动的模拟-一种在计算域的入口处具有均匀(理想)的速度分布,另一种具有通过实验确定的速度分布。在理想边界条件下进行的模拟产生的结果较差,与实验测量值之间存在很大差异。另一方面,当使用真实的(测量的)边界条件时,模拟产生了更准确的结果。边界条件的影响可以在水翼附近的x和y速度分量,水翼表面上的c(p)分布以及入口下游速度分布的演变中看到。得出的结论是,如果需要精确的模拟结果,则必须使用真实的(测得的)速度曲线作为入口边界条件,或者确保真实的上游流量几乎理想地均匀。 (C)2007 Elsevier Inc.保留所有权利。

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