论文标题
螺旋桨尖端涡流缓解粗糙度应用
Propeller Tip Vortex Mitigation By Roughness Application
论文作者
论文摘要
在这项研究中,评估了表面粗糙度在模型和全尺寸海洋螺旋桨上的应用,以减轻尖端涡流空化。为了建模湍流,采用SST komegamodel以及曲率校正来模拟在适当的网格分辨率上进行尖端涡流传播的流量,根据我们以前的指南,每个涡流直径至少32个单元。粗糙度的效果是通过修饰的壁功能建模的。该分析的重点是在海洋螺旋桨上出现的两种类型的涡流:尖端涡流以较低的前进比数和领先的尖端涡流以较高的提前比例发展。结果表明,随着这两种类型的涡流的起源和形成不同,需要不同的粗糙度模式来减轻螺旋桨性能的性能降解。我们的发现阐明,在刀片尖端上具有粗糙度的结合以及前缘有限的区域是最佳的粗糙度模式,在这些模式下,可以实现尖端涡流空化缓解和性能退化之间合理平衡。模型量表条件下的这种模式导致平均TVC减轻37%,平均性能降解为1.8%,而在全尺度条件下,平均TVC减轻22%,性能降解为1.4%。
In this study, the application of surface roughness on model and full scale marine propellers in order to mitigate tip vortex cavitation is evaluated. To model the turbulence, SST kOmegamodel along with a curvature correction is employed to simulate the flow on an appropriate grid resolution for tip vortex propagation, at least 32 cells per vortex diameter according to our previous guidelines. The effect of roughness is modeled by modified wall functions. The analysis focuses on two types of vortices appearing on marine propellers: tip vortices developing in lower advance ratio numbers and leading-edge tip vortices developing in higher advance ratio numbers. It is shown that as the origin and formation of these two types of vortices differ, different roughness patterns are needed to mitigate them with respect to performance degradation of propeller performance. Our findings clarify that the combination of having roughness on the blade tip and a limited area on the leading edge is the optimum roughness pattern where a reasonable balance between tip vortex cavitation mitigation and performance degradation can be achieved. This pattern in model scale condition leads to an average TVC mitigation of 37% with an average performance degradation of 1.8% while in full scale condition an average TVC mitigation of 22% and performance degradation of 1.4% are obtained.