CFD Analysis of a Round Shaped Air Cushion Vehicle with Flexible Skirt Segments at 90° Part I: Different Positions of Bag to Cushion Feed Orifice

M. Pavăl, A. Popescu, D. Zahariea
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Abstract

Abstract Air cushion vehicles represent an interesting research area, mainly from their application point of view. But, at the same time, represents the reason of the scarcity of published results. Based on a series of initial simulations carried out by authors, which analysed lift forces for a round-shaped air cushion vehicle where the segments of the flexible skirt were inclined at 90˚, it was decided to carry out more complex studies regarding this configuration, presented in a series of articles. This complex study consists in performing static CFD simulations, in which values for different constructive elements are modified in order to analyse their influence on lift force. In this first article, the imposed fixed parameters are: angle of inclination of the segments of the flexible skirt and height of the segments, respectively. The main constructive variable parameters are: air clearance height and length between the edge of the bag to cushion feed orifice and inner wall of the flexible skirt segments. The simulations were carried out in ANSYS Fluent software, where velocity contours, streamlines and velocity profiles from the exit under the flexible skirt were analysed and through Curve Fitting Toolbox application found in MATLAB program, the equations were established that describe lift force variation.
带有90°柔性裙段的圆形气垫飞行器的CFD分析第一部分:气囊与气垫进给孔的不同位置
摘要气垫车辆是一个有趣的研究领域,主要是从其应用角度来看。但同时也代表了发表成果稀缺的原因。基于作者进行的一系列初步模拟,分析了圆形气垫飞行器在柔性裙段呈90°倾斜时的升力,决定对这种配置进行更复杂的研究,并在一系列文章中提出。这项复杂的研究包括进行静态CFD模拟,其中修改不同构造元素的值以分析它们对升力的影响。在第一篇文章中,施加的固定参数分别为:柔性裙段的倾角和段的高度。主要构造变量参数为:气囊边缘到缓冲进料孔和柔性裙段内壁之间的空气间隙高度和长度。在ANSYS Fluent软件中进行了仿真,分析了柔性裙下出口的速度轮廓线、流线和速度剖面,并通过MATLAB程序中的曲线拟合工具箱建立了升力变化方程。
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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