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Geometric Filtration Using Proper Orthogonal Decomposition for Aerodynamic Design Optimization

机译:使用正确正交分解进行几何过滤以优化空气动力学设计

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摘要

When carrying out design searches, traditional variable screening techniques can find it extremely difficult to distinguish between important and unimportant variables. This is particularly true when only a small number of simulations are combined with a parameterization that results in a large number of variables of seemingly equal importance. Here, the authors present a variable reduction technique that employs proper orthogonal decomposition to filter out undesirable or badly performing geometries from an optimization process. Unlike traditional screening techniques, the presented method operates at the geometric level instead of the variable level. The filtering process uses the designs that result from a geometry parameterization instead of the variables that control the parameterization. The method is shown to perform well in the optimization of a two-dimensional airfoil for the minimization of drag-to-lift ratio, producing designs better than those resulting from traditional kriging-based surrogate model optimization and with a significant reduction in surrogate tuning cost
机译:在进行设计搜索时,传统的变量筛选技术会发现很难区分重要变量和不重要变量。当仅将少量模拟与参数化组合使用,导致大量看似同等重要的变量时,情况尤其如此。在这里,作者提出了一种可变约简技术,该技术采用适当的正交分解来从优化过程中滤除不良或性能不佳的几何形状。与传统的筛选技术不同,本文提出的方法在几何级别而不是可变级别上运行。过滤过程使用由几何参数化产生的设计,而不是控制参数化的变量。该方法在二维翼型的优化中表现出了很好的效果,以最小化阻力比,与传统的基于克里格法的替代模型优化相比,所产生的设计效果更好,并且显着降低了替代调整成本

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