首页> 外文期刊>Brodogradnja >INVESTIGATION OF HYDROELASTIC BEHAVIOR OF A PONTOON-TYPE VLFS DURING UNSTEADY EXTERNAL LOADS IN WAVE CONDITION USING A HYBRID FINITE ELEMENT-BOUNDARY ELEMENT (FE-ME) METHOD
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INVESTIGATION OF HYDROELASTIC BEHAVIOR OF A PONTOON-TYPE VLFS DURING UNSTEADY EXTERNAL LOADS IN WAVE CONDITION USING A HYBRID FINITE ELEMENT-BOUNDARY ELEMENT (FE-ME) METHOD

机译:混合有限元-边界元(FE-ME)法研究波状VLFS在波浪状态下非定常外部载荷作用下的水弹性行为

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The hydroelastic behaviour of a pontoon-type VLFS subjected to unsteady external loads in wave condition is investigated in the context of the time-domain modal expansion theory, in which the boundary element method (BEM) based on time domain Kelvin sources is used for hydrodynamic forces and the finite element method (FEM) is adopted for solving the deflections of the VLFS. In this analysis, the interpolation-tabulation scheme is applied to assess rapidly and accurately the free-surface Green function in finite water depth, and the boundary integral equation of a quarter VLFS model is further established taking advantage of symmetry of flow field and structure. The VLFS is modelled as an equivalent solid plate based on the Mindlin plate theory. The coupled plate-water model is performed to determine the wave-induced responses and transient behaviour under external loads such as a huge mass impact onto the structure and moving loads of an airplane, respectively. These results are verified with existing numerical results and experimental test. Then, the developed numerical tools are used in the study of the combined action taking into account of the mass drop/airplane landing as well as forward or reverse incident wave action. The deflections of the runway, the time history of vertical positions and the trajectory of the airplane are also presented through a systematic time-domain simulation, which illustrates the usefulness of the presently developed numerical solutions.
机译:在时域模态扩展理论的背景下,研究了浮体型VLFS在波浪条件下承受非稳态外部载荷的水弹性行为,其中基于时域开尔文源的边界元方法(BEM)被用于流体力学。力和有限元方法(FEM)用于解决VLFS的挠度。在此分析中,采用插值制表法来快速,准确地评估有限水深中的自由表面格林函数,并利用流场和结构的对称性进一步建立了四分之一VLFS模型的边界积分方程。根据Mindlin板理论,VLFS被建模为等效实体板。执行耦合的板水模型来确定在外部负载(例如分别对飞机结构的巨大质量冲击和飞机的移动负载)下的波浪感应响应和瞬态行为。这些结果已通过现有的数值结果和实验测试得到了验证。然后,在考虑到质量下降/飞机着陆以及正向或反向入射波作用时,将开发的数值工具用于组合作用的研究。还通过系统的时域仿真来显示跑道的偏转,垂直位置的时程和飞机的轨迹,这说明了当前开发的数值解的有用性。

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