Optimization Design of an Blended Wing Body Underwater Glider's Configuration

Qiaogao Huang, Guanshan Liu, Yunlong Ma, G. Pan, Da Lv
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Abstract

For the blended-wing-body underwater gliders, lift-to-drag ratio which is mainly determined by the profile foils is one of the most important performance parameters. In this paper, GUI functions based on MATLAB code are applied to form an optimization system. Parametric model of the foil are described by Class function/shape function transformation (CST) method. XFOIL, an open-source code is employed to compute the hydrodynamic performance of the profile foils. Genetic algorithm is used to finish the optimization of the foils which derived from the profiles of one original blended-wing-body underwater gliders. The optimization result showed that the lift-to-drag ratio of the profile foils rises up to 36%. By using the optimized foils, the new blended-wing-body underwater glider gets its improvements in maximum lift-to-drag ratio, range of attack angle with high lift-to-drag ratio and payload capacity.
混合翼体水下滑翔机构型优化设计
对于翼身混合型水下滑翔机来说,升阻比是其最重要的性能参数之一,而升阻比主要由翼型翼片决定。本文采用基于MATLAB代码的GUI函数组成优化系统。采用类函数/形函数变换(CST)方法描述了金属箔的参数化模型。利用开放源代码XFOIL计算了叶型的水动力性能。利用遗传算法对原翼体混合型水下滑翔机的翼型进行优化设计。优化结果表明,该型箔的升阻比提高到36%。采用优化后的翼身混合型水下滑翔机,在最大升阻比、大升阻比攻角范围和有效载荷能力等方面得到了改善。
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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