Numerical Research on the Influence of Interceptor Flaps on the Planing Hydrodynamic Performance

IF 0.7 Q4 ENGINEERING, MARINE Nase More Pub Date : 2023-10-01 DOI:10.17818/nm/2023/4.4
Samuel Samuel, Serliana Yulianti, Parlindungan Manik, Andi Trimulyono, Ahmad Firdhaus, Tuswan Tuswan, Dian Purnama Sari
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Abstract

The trim tab and interceptor have been utilized to optimize the running trim and motion control of planing boats at varying speeds in calm water. Increasing the height of the interceptor can create excessive drag and bow-down trim. The effectiveness of the interceptor can be increased by integrating it with a horizontal flap. This research focuses on the impact of the influence caused by interceptor flaps on the pressure distribution and fluid flows around the vessel. To simulate trim and sinkage measurement, the environment was modeled in the two-degree of freedom condition. Variation of integrated interceptor flaps has been analyzed with Finite Volume Method (FVM) based on RANS (Reynolds-Averaged Navier-Stokes) equation using overset mesh. The turbulent K- ε and VOF (Volume of Fluid) models are used to model the water and air phases. The grid convergence study is performed to establish the parallel solver’s grid independence. To confirm the accuracy of the test in the bare hull condition, the numerical approach was tested experimentally. The result of drag, trim, and sinkage was calculated and it has been proved that the added flaps into interceptors are very useful in drag reduction and trim control. The percentage of interceptor height is directly proportional to the resulting lift force. Higher lift force can more effectively improve trim and reduce drag. Overall, this study shows an improvement in ship performance when using an interceptor and interceptor flap. One of the model configurations in the study has been shown to reduce drag by up to 33.3% at Froude number 1.45 when compared to ships without an interceptor.
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截流襟翼对平面水动力性能影响的数值研究
在平静的水面上,利用纵倾卡和拦截器来优化平滑船在不同速度下的运行纵倾和运动控制。增加拦截器的高度会产生过大的阻力和俯身修剪。拦截器的有效性可以通过将其与水平襟翼集成来提高。本文研究的重点是截流襟翼对压力分布和容器周围流体流动的影响。为了模拟纵倾和下沉测量,在二自由度条件下对环境进行建模。采用基于reynolds - average Navier-Stokes方程的有限体积法(FVM),利用overset网格分析了集成截击机襟翼的变化。湍流K- ε和VOF(流体体积)模型被用来模拟水和空气的相。通过网格收敛性研究,建立了并行求解器的网格独立性。为了验证该数值方法在裸壳工况下的准确性,对该数值方法进行了实验验证。计算了阻力、纵倾和下沉的结果,证明了在截流器中增加襟翼对减阻和纵倾控制是非常有用的。拦截器高度的百分比与产生的升力成正比。更高的升力可以更有效地改善纵倾和减少阻力。总的来说,本研究表明,当使用拦截弹和拦截弹襟翼时,舰船性能有所改善。研究中的一种模型配置显示,与没有拦截器的船舶相比,在弗鲁德数1.45处阻力减少高达33.3%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Nase More
Nase More ENGINEERING, MARINE-
CiteScore
1.90
自引率
22.20%
发文量
17
审稿时长
15 weeks
期刊最新文献
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