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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.
概括
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.
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.
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