冲击平面倾斜度对翔空气动力学性能上的影响 双重翻拍片的悬空性能
Shubham Tiwari1, Sunil Chandel1
1Department of Mechanical Engineering, Defence Institute of Advanced Technology (DU), Girinagar, Pune 411025, Maharashtra, India.
Bioinspiration & biomimetics
|January 4, 2024
概括
龙飞行依赖于独立的机翼控制. 数字模拟显示,非平行翼冲动平面可以显著增加起重,为微型空中车辆设计提供了洞察力.
科学领域:
- 流体动力学 流体动力学
- 空气动力学 航空动力学
- 生物启发的工程是生物启发的工程.
背景情况:
- 龙和蝶表现出了非凡的飞行敏捷性和耐力.
- 这种能力归因于它们四个翅膀的独立动力控制.
- 了解昆虫的飞行机制可以为先进的飞行器的设计提供信息.
研究的目的:
- 为了研究冲击平面角度对动翼的空气动力学性能的影响.
- 分析平行与非平行冲程平面对起重和推力的影响.
- 探索振荡翅膀之间的相位差异的影响.
主要方法:
- 在157.7的雷诺兹数 (Re) 时,对两个并列气体的数值模拟.
- 沿着倾斜的冲击平面振荡的气形.
- 不同的冲平面角度 (β) 和相差 (φ = 0°,90°,180°).
主要成果:
- 对于平行冲动平面,增加冲动平面角 (β) 增加了升力,但减小了推力.
- 提升和推力通常随着相差 (φ) 的增加而减少.
- 非平行冲动平面在φ=0°和90°时对升力产生负面影响,但在φ=180°时观察到46%的升力增大,当前翼角较小时.
结论:
- 机翼动力学,特别是冲击平面角度和相位差异,极大地影响了空气动力学性能.
- 在特定条件下 (φ = 180°),非平行冲程平面可以增强升力.
- 这些发现为优化微型空中飞机机翼设计提供了宝贵的数据.
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