Hydrodynamic performance analysis of podded propulsor under ice blockage condition 冰阻塞状态下吊舱推进器水动力性能分析

Chun-yu Guo, Pei Xu, Lianzhou Wang, Wanzhen Luo
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引用次数: 5

摘要

为了分析冰阻塞条件下l型吊舱推进器的水动力性能和流场特性,基于RANS方法,采用重叠网格技术对l型吊舱推进器在不同螺旋桨与冰距离下的非定常水动力性能进行了数值计算。研究结果表明:随着螺旋桨与冰的距离减小,螺旋桨与吊舱单元的推力和扭矩逐渐增大,距离较近时增加较快,但增加值不稳定;随着螺旋桨与冰间距离的减小,阻塞区叶片压差逐渐增大,而其他叶片压差基本不变,支板与吊舱压差增大。螺旋桨与冰之间的阻塞区轴向入流速度先减小后增大再减小,非阻塞区轴向入流速度基本不变。螺旋桨尾涡高速区沿螺旋桨旋转方向逐渐增大。
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Hydrodynamic performance analysis of podded propulsor under ice blockage condition 冰阻塞状态下吊舱推进器水动力性能分析
In order to analyze the hydrodynamic performance and flow field characteristics of L-type podded propulsor under ice blockage condition, based on the RANS method, the unsteady hydrodynamic performance of L-type podded propulsor at different distances between propeller and ice was numerically calculated by using the overlapping grid technology.Research results show that with the decrease of the distance between propeller and ice, thrust and torque of propeller and pod unit increase gradually, and rapid increase when the distance is near, but the added value is unstable.With the decrease of the distance between propeller and ice, blade pressure difference increases gradually in blocking region, while the other blade pressure differences are almost the same, and the pressure differences of the strut and pod increase.The axial inflow velocity in the blocking region between the propeller and ice decreases first, then increases, and then decreases, and the axial inflow velocity is almost constant in the non-blocking zone.The high velocity area of the propeller trailing vortex increases gradually towards the propeller rotation direction.
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