基于CFD的设计优化,使用Taguchi方法在混合翼机身机身上诱导的穴,使用Taguchi方法
Haris Ali1, Mohammad Rasidi Rasani1, Zambri Harun1
1Department of Mechanical and Manufacturing Engineering, Faculty of Engineering and Built Environment, Universiti Kebangsaan Malaysia (UKM), Bangi, Selangor, Malaysia.
PloS one
|April 17, 2025
概括
在混合翼机身 (BWB) 机身上优化孔设计可以提高空气动力学效率. 孔直径显著影响阻力和提升至阻力比率,指导被动流量控制策略.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 空气动力学 在空气动力学.
背景情况:
- 被动流量控制方法对于提高飞机空气动力学效率至关重要.
- 泡是飞机机体的一个有前途的被动流量控制技术.
- 优化洞穴几何学是最大限度地提高它们有效性的关键.
研究的目的:
- 为了优化混合翼机身 (BWB) 机身上的小穴的设计.
- 为了研究各种穴设计参数对空气动力学性能的影响.
- 为了确定最佳的孔配置,以改善提升-拖拉比率.
主要方法:
- 实验设计 (DOE) 框架使用塔古奇方法.
- 使用L18直角阵列来测试18个配置.
- 进行高保真计算流体动力学 (CFD) 模拟以进行空气动力学分析.
- 应用信号噪声比 (SNR) 和帕雷托差异分析 (ANOVA) 用于数据解释.
主要成果:
- 孔直径是对阻力系数 (CD) 和提升至阻力比 (L/D) 最有影响力的参数.
- 洞穴深度对空气动力学性能的影响最小.
- 确定了一个最优的沟设计变量组合 (A1B1C1D3E3),以最大限度地减少CD和最大限度地增加L/D.
结论:
- 孔设计优化显著提高了BWB机身的空气动力效率.
- 孔径是有效的被动流量控制的关键因素.
- 这些发现为航空航天领域的应用提供了实际指导方针.
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