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Efficient computation of the POD manifold containing the information required to generate a multi-parameter aerodynamic database

机译:POD歧管的高效计算,其中包含生成多参数空气动力学数据库所需的信息

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摘要

A method is presented to calculate efficiently the proper orthogonal decomposition (POD) manifold (spanned by POD modes) that contains the information needed to generate a multi-parameter aerodynamic database. This work is motivated by the need, driven by market competition, to improve the efficiency of both aerodynamic design and analysis processes in the aeronautic sector. Current aerodynamic database generation is carried out in industry performing CFD computations at the nodes of a dense Cartesian grid in the parameter space. This approach does not account for the redundancies that are necessarily involved and, therefore, it is not the most efficient from the points of view of computational cost and time needed to generate the database. Such redundancies are an advantage when generating the database by means of the (already described in the literature) reduced order models based on projection of the governing equations on a POD manifold, which must be previously calculated from a set of CFD computed snapshots. The method proposed in this paper provides such POD manifold with a small number of snapshots, comparable to the dimension of the POD manifold itself, which is a crucial step for the computational efficiency of the proposed database generation method. The method is tested considering the aerodynamic flow around a horizontal tail plane (HTP) in the parameter range 0.4 ≤ Mach number ≤ 0.8 and —3° ≤ angle of attack ≤ 3°, obtaining the POD manifold with a good precision using 20, conveniently selected snapshots.%Aerospace Propulsion and Fluid Dynamics Department, School of Aeronautics, Universidad Politecnica de Madrid, Plaza del Cardenal Cisneros 3,28040 Madrid, Spain;Applied Mathematics Department, School of Aeronautics, Universidad Politecnica de Madrid, Plaza del Cardenal Cisneros 3,28040 Madrid, Spain;Aerospace Propulsion and Fluid Dynamics Department, School of Aeronautics, Universidad Politecnica de Madrid, Plaza del Cardenal Cisneros 3,28040 Madrid, Spain;
机译:提出了一种方法,可以有效地计算适当的正交分解(POD)流形(由POD模式跨越),其中包含生成多参数空气动力学数据库所需的信息。这项工作的动机是在市场竞争的推动下,需要提高航空领域的空气动力学设计和分析过程的效率。当前的空气动力学数据库生成是在行业中在参数空间中密集的笛卡尔网格的节点上执行CFD计算时执行的。这种方法没有考虑到必须涉及的冗余,因此,从生成数据库所需的计算成本和时间的角度来看,它不是最有效的。当基于(已经在文献中描述过)基于控制方程在POD流形上的投影的降阶模型生成数据库时,这种冗余是一个优势,必须事先从一组CFD计算的快照中计算出这些冗余。本文提出的方法为POD流形提供了少量快照,可与POD流形本身的尺寸相比,这是所提出的数据库生成方法的计算效率的关键步骤。该方法在参数范围0.4≤马赫数≤0.8和-3°≤攻角≤3°的参数范围内,围绕水平尾翼(HTP)的气动流动进行了测试,使用20即可方便地获得POD歧管马德里理工大学航空学院航空推进与流体动力学系,西班牙马德里卡斯蒂纳尔·西斯内罗斯广场3,28040;马德里理工大学航空学院应用数学系,西班牙广场·卡森纳尔·西斯内罗斯3 28040西班牙马德里;马德里理工大学航空学院航空航天推进和流体动力学系,西班牙西德内罗广场328040;西班牙马德里;

著录项

  • 来源
    《Aerospace science and technology》 |2013年第1期|152-160|共9页
  • 作者单位

    Aerospace Propulsion and Fluid Dynamics Department, School of Aeronautics, Universidad Politecnica de Madrid, Plaza del Cardenal Cisneros 3,28040 Madrid, Spain;

    Applied Mathematics Department, School of Aeronautics, Universidad Politecnica de Madrid, Plaza del Cardenal Cisneros 3,28040 Madrid, Spain;

    Aerospace Propulsion and Fluid Dynamics Department, School of Aeronautics, Universidad Politecnica de Madrid, Plaza del Cardenal Cisneros 3,28040 Madrid, Spain;

  • 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

    proper orthogonal decomposition (POD); design of experiments (DOE); aerodynamics; database; snapshots selection; sequential sampling;

    机译:适当的正交分解(POD);实验设计(DOE);空气动力学数据库;快照选择;顺序采样;
  • 入库时间 2022-08-18 02:33:13

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