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相关实验视频

Updated: May 22, 2025

Design and Optimization Strategies of a High-Performance Vented Box
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使用细胞自动机参数化的拓包括空气动力学形状优化.

M J Wood1, T C S Rendall1, C B Allen1

  • 1Department of Aerospace Engineering, University of Bristol, Bristol, BS8 1TR UK.

Structural and multidisciplinary optimization : journal of the International Society for Structural and Multidisciplinary Optimization
|March 17, 2025
PubMed
概括
此摘要是机器生成的。

一种新方法使用细胞自动机来创建复杂的空气动力学形状. 这种几何参数化准确地重建了气翼,并设计了多体超音速几何形状,显著减少了阻力.

关键词:
空气动力学拓优化优化蜂自动机是一个自动机.优化 优化 优化参数化的参数化

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科学领域:

  • 计算流体动力学 计算流体动力学
  • 航空航天工程是航空航天工程.
  • 几何建模的几何建模.

背景情况:

  • 复杂的几何形状在空气动力学设计中带来了挑战.
  • 现有的参数化方法对于任意拓可能缺乏灵活性.
  • 优化多对象空气动力学配置需要先进的工具.

研究的目的:

  • 介绍一种由细胞自动机驱动的新型几何参数化方法.
  • 为了能够描述具有任意拓的复杂几何形状.
  • 为了优化空气动力学形状以减少阻力,特别是在超音速流程中.

主要方法:

  • 一种体积固体驱动的细胞自动机方法用于几何参数化.
  • 接近平滑,最小表面积几何形状与局部体积约束.
  • 使用具有适应性改进能力的几何控制网格.
  • 采用无梯度优化用于空气动力学形状设计.

主要成果:

  • 在容忍范围内成功重建了超过98%的气翼几何体.
  • 在超音速流量条件下恢复已知的分析最佳值.
  • 构建多体空气动力学几何形状,与单体最佳相比,阻力显著降低.

结论:

  • 开发的参数化方法有效地处理复杂的空气动力学形状.
  • 它可以设计高性能多体超音速配置.
  • 这种方法为空气动力学优化和设计提供了一个强大的工具.