Numerical Research on Impacting Load and Structural Response for a Model Experiment of High-speed Craft

Weiqin Liu, Yuxin Qin, Yuchen Hu, Nikola Vladimir, Shuangxi Xu, Yigang Wu
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Abstract

High-speed craft generally applies hy droplane boat-type and large power engine to obtain high speed in water as results that significant hydrodynamic nonlinearities, high-speed craft has complex the impact load characteristics and structural response which attract considerable attentions of ship mechanics researchers. This paper studies impacting load and structural response of a high-speed craft by means of numerical approach coupling CFD and FEM. A model experiment of high-speed craft is selected to simulate impact load and structural response, the craft model consists of two ship bodies and a keel beam, a number of pressure sensors and strain gauges are arranged to capture the impacting pres s ure and VBM. A numerical FSI approach coupling CFD and FEM is used to study the model experiment of the high-speed craft. CFD is used to solve the hydrodynamics of the high-speed craft, DFBI and overset grid algorithm are employed to simulate the craft motion. Dy namic FEM is us ed to calculate structural response of high-speed craft, structural VBM is obtained. Two-way FSI is employ ed to realize coupling of CFD and FEM, wave pres s ures and structural displacement are iterated to progress. At last, numerical res ults and experimental res ults including impacting pressure, craft motion and VBM are compared and analyzed, they agree with closely. The numerical approach can be used to study the impacting load and structural respons e for high-speed craft.
高速飞船撞击载荷与结构响应模型试验数值研究
高速船一般采用斜面船型和大功率发动机在水中获得较高的速度,由于显著的水动力非线性,高速船具有复杂的冲击载荷特性和结构响应,这引起了船舶力学研究人员的极大关注。本文通过将 CFD 和 FEM 相结合的数值方法研究了高速船的冲击载荷和结构响应。选取高速船模型试验来模拟冲击载荷和结构响应,船模由两个船体和一个龙骨梁组成,布置了多个压力传感器和应变片来捕捉冲击预态和 VBM。采用 CFD 和 FEM 相结合的 FSI 数值方法来研究高速船的模型试验。CFD 用于求解高速飞行器的流体力学,DFBI 和超集网格算法用于模拟飞行器的运动。利用动态有限元计算高速飞行器的结构响应,得到结构 VBM。采用双向 FSI 实现 CFD 与 FEM 的耦合,对波浪预报和结构位移进行迭代。最后,将数值结果与实验结果(包括冲击压力、飞艇运动和 VBM)进行对比分析,结果非常吻合。该数值方法可用于研究高速飞行器的冲击载荷和结构响应。
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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