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Reduced-Order Modeling of Complex Aerodynamic Geometries Using Canonical Shapes

机译:使用规范形状对复杂的空气动力学几何形状进行降阶建模

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The aerodynamics of bluff bodies are of interest in several engineering applications. The numerical prediction of the behavior of these geometries requires high fidelity approaches, the cost of which increases with the complexity of the body of interest. Thus, design and modeling and simulation solvers are usually limited to surrogate data on canonical shapes and/or estimates based on flat plate drag area. A new concept, the COMPlex Aerodynamic Shape Simulator (COMPASS), is proposed to estimate the quasi-steady aerodynamic coefficients for arbitrary configurations, which can then be applied in unsteady reduced-order models and design software. This approach decomposes complex shapes into an aggregate of canonical bodies, and then computes the aerodynamic characteristics of the complex geometry from the separation and reattachment properties of the relevant canonical shapes. This paper introduces the initial method which applies a rectangular bluff body as the canonical shape. The baseline COMPASS has been analyzed on one canonical shape (rectangular prism), and two complex configurations (truck and trailer). The resulting aerodynamic properties have been compared with Computational Fluid Dynamics (CFD) and experimental data. COMPASS is shown to be a viable concept for the estimation of the quasi-steady aerodynamic loads of the complex shapes analyzed. Additional on-going development of COMPASS is also summarized.
机译:钝体的空气动力学在一些工程应用中是令人感兴趣的。对这些几何形状的行为进行数值预测需要高保真度的方法,其成本会随着目标物体的复杂性而增加。因此,设计,建模和仿真求解器通常仅限于替代规范形状的数据和/或基于平板拖曳面积的估计值。提出了一种新概念COMPLEX空气动力学形状仿真器(COMPASS)来估计任意配置的准稳态空气动力学系数,然后将其应用于非稳态降阶模型和设计软件中。这种方法将复杂形状分解为规范实体的集合,然后根据相关规范形状的分离和重新附着属性来计算复杂几何形状的空气动力学特性。本文介绍了将矩形钝体作为规范形状的初始方法。基准COMPASS已在一种规范形状(矩形棱柱)和两种复杂配置(卡车和拖车)上进行了分析。所得的空气动力学特性已与计算流体动力学(CFD)和实验数据进行了比较。 COMPASS被证明是一种可行的概念,可用于评估所分析的复杂形状的准稳态空气动力载荷。还总结了COMPASS正在进行的其他开发。

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