通过使用小穴进行被动的流场控制,以改善机翼上的空气动力学流量
Haris Ali1, Mohammad Rasidi Rasani2, Zambri Harun3
1Department of Mechanical and Manufacturing Engineering, Faculty of Engineering and Built Environment, Universiti Kebangsaan Malaysia (UKM), 43600, Bangi, Selangor, Malaysia. P119583@siswa.ukm.edu.my.
Scientific reports
|June 5, 2024
概括
在直立的矩形翅膀上的穴可以通过保持附着的空气流来减少高达6.6%的阻力. 这种空气动力学增强可以提高机翼性能,而不会显著改变起重.
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
- 应用物理 应用物理
背景情况:
- 起重表面的空气动力学性能在航空航天应用中至关重要.
- 流量分离和拖动是机翼设计中的关键挑战.
- 表面修改提供了性能提升的潜力.
研究的目的:
- 为了研究形配置在直立矩形翼上的空气动力学效应.
- 量化由于孔表面造成的阻力和升力系数的变化.
- 分析流场并了解性能变化背后的机制.
主要方法:
- 使用了计算流体动力学 (CFD) 模拟.
- 使用了k-ω剪切应力传输 (SST) 流模型.
- 数值结果与实验数据和先前的模拟数据进行了验证.
主要成果:
- 缩的翼面降低了多达6.6%的阻力系数 (CD).
- 孔隙有助于维持附着的空气流,延迟流量分离.
- 升力系数 (CL) 显示,随着的结合,升力系数的变化是可以忽略不计的.
结论:
- 孔表面显著提高了机翼的空气动力学性能.
- 在空气动力学设计中,隙为减少阻力提供了一种可行的策略.
- 这项研究证实了小穴在改善提升-拖拉比率方面的有效性.
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