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Active Subspaces of Airfoil Shape Parameterizations

机译:翼型形状参数化的活动子空间

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摘要

Design and optimization benefit from understanding the dependence of a quantity of interest (e.g., a design objective or constraint function) on the design variables. A low-dimensional active subspace, when present, identifies important directions in the space of design variables; perturbing a design along the active subspace associated with a particular quantity of interest changes that quantity more, on average, than perturbing the design orthogonally to the active subspace. This low-dimensional structure provides insights that characterize the dependence of quantities of interest on design variables. Airfoil design in a transonic flowfield with a parameterized geometry is a popular test problem for design methodologies. Two particular airfoil shape parameterizations are examined (parametric sections and class-shape transformation), and the active subspaces present in two common design quantities of interest (transonic lift and wave-drag coefficients) are studied under each shape parameterization. The two parameterizations are mathematically related by a simple change of variable and subsequent odd-power polynomial series. The active subspaces enable low-dimensional approximations of lift and drag that relate to physical perturbations of the airfoil, In particular, a two-dimensional approximation of both transonic lift and drag is obtained and interpreted, where 1) each dimension is a particular linear combination of the design variables resulting in intuitive airfoil perturbations, and 2) the linear combination weights are related between lift and drag, ft is shown how these approximations along with similarities between the lift and drag active subspaces inform a multi-objective design problem.
机译:设计和优化得益于理解感兴趣的量(例如,设计目标或约束函数)对设计变量的依赖性。低维活动子空间(如果存在)可标识设计变量空间中的重要方向。沿着与特定数量的关注对象关联的活动子空间对设计进行扰动,与对正交于活动子空间的正交设计进行扰动相比,平均改变的数量更多。这种低维结构提供了洞察力,这些洞察力表征了感兴趣的数量对设计变量的依赖性。跨音速流场中具有参数化几何形状的机翼设计是设计方法中的一个普遍测试问题。检查了两个特定的机翼形状参数化(参数截面和类形状转换),并且在每个形状参数化下研究了两个共同感兴趣的设计量(跨音速升力和波阻系数)中存在的活动子空间。这两个参数化在数学上通过简单的变量变化和随后的奇次幂多项式级数相关。活动子空间实现了与机翼的物理扰动有关的升力和阻力的低维近似,特别是,获得并解释了跨音速升力和阻力的二维近似,其中1)每个维都是特定的线性组合设计变量导致直观的机翼扰动; 2)升力和阻力之间的线性组合权重相关联,ft显示了这些近似值以及升力和阻力有效子空间之间的相似性如何解决了多目标设计问题。

著录项

  • 来源
    《AIAA Journal》 |2018年第5期|2003-2017|共15页
  • 作者单位

    Univ Colorado, Aerosp Engn Sci Dept, Boulder, CO 80309 USA;

    Univ Colorado, Dept Comp Sci, Boulder, CO 80309 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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