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SPH numerical investigation of the velocity field and vorticity generation within a hydrofoil-induced spilling breaker

机译:水翼诱发溢流破碎锤内速度场和涡度产生的SPH数值研究

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In the present work, the velocity field and the vorticity generation in the spilling generated by a NACA 0024 hydrofoil were studied. SPH simulations were obtained by a pseudo-compressible XSPH scheme with pressure smoothing; both an algebraic mixing-length model and a two-equation model were used to represent turbulent stresses. Given the key role of vortical motions in the generation of the spilling breaker, the sources of vorticity were then examined in detail to confirm the interpretation of the mean flow vortical dynamics given in a paper by Dabiri and Gharib (J Fluid Mech 330: 113-139, [ 1997]). The high precision of the SPH model is confirmed through a comparison with experimental data. Experimental investigations were carried out by measuring the velocity field with a backscatter, two-component four-beam optic-fiber LDA system. The agreement between the numerical results and laboratory measurements in the wake region is satisfactory and allows the evaluation of the wave breaking efficiency of the device by a detailed analysis of the simulated flow field.
机译:在目前的工作中,研究了由NACA 0024水翼产生的溢流中的速度场和涡旋产生。 SPH模拟是通过具有压力平滑的拟可压缩XSPH方案获得的。代数混合长度模型和二方程模型都用来表示湍流应力。考虑到涡旋运动在溢出破碎器产生中的关键作用,然后详细检查涡旋源,以确认Dabiri和Gharib在一篇论文中给出的平均流涡旋动力学的解释(J Fluid Mech 330:113- 139,[1997]。通过与实验数据的比较证实了SPH模型的高精度。通过使用反向散射,两分量四光束光纤LDA系统测量速度场来进行实验研究。数值结果与尾流区域的实验室测量结果之间的一致性令人满意,并且可以通过对模拟流场的详细分析来评估设备的破波效率。

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