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Experimental and Numerical Research on the Influence of Stern Flap Mounting Angle on Double-Stepped Planing Hull Hydrodynamic Performance

机译:船尾襟翼安装角度对双级滑行船体水动力性能影响的实验与数值研究

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In the current hydrodynamic research relating to planing hulls, the stern flap and steps are generally considered to be two independent resistance reduction measures. Limited research has focused on the coupled effects of flaps and steps. Therefore, experimental and numerical simulation methods are carried out in this paper to explore the influence of the flap mounting angle coupled with the steps. A series of model towing tests were implemented for a double-stepped planing hull with 2°, 3° and 4.5° flap angles. The test results show that, as the mounting angle increased, the low speed resistance performance was improved and the porpoising critical speed was delayed, with a slight resistance cost. Based on the tests, a numerical simulation method was established with volume Froude numbers ranging from 0.88 to 5.20. The simulated hull flow field showed good agreement with the testing data. The simulation results suggest a cavity induces the negative pressure after the steps; the cavity core region is the air phase, and this expands with the air–water mixture flow. The cavity also causes wetted surface reduction and pressure distribution changes. Finally, comparisons of cavities after-steps and load coefficients of different planing surfaces among models were considered. Numerical results analysis gave distinct interpretations for the experimental phenomenon of porpoising critical speed increasing with a slight resistance increment.
机译:在当前有关滑行船体的水动力研究中,船尾襟翼和踏板通常被认为是两个独立的阻力减小措施。有限的研究集中在襟翼和踏板的耦合作用上。因此,本文进行了实验和数值模拟方法,以探讨襟翼安装角度和台阶的影响。对具有2°,3°和4.5°襟翼角的双台阶滑行船体进行了一系列模型拖曳测试。测试结果表明,随着安装角度的增加,低速阻力性能得到改善,而致密化临界速度被延迟,阻力成本略有降低。基于这些测试,建立了数值模拟方法,其体积弗劳德数范围为0.88至5.20。模拟的船体流场与试验数据吻合良好。仿真结果表明,在这些步骤之后,空腔会引起负压;空腔的核心区域是空气相,并且随着空气-水混合物的流动而膨胀。该腔还导致润湿的表面减少和压力分布变化。最后,考虑了模型之间不同平面的型腔后台阶和载荷系数的比较。数值结果分析给出了对poropising临界速度随轻微阻力增加而增加的实验现象的独特解释。

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