翅膀等离子体冰形调节的优化方法基于对飞行风险的定量评估
Zhe Li1, Pengfei Dou2, Qiao Huang2
1Aviation Engineering School, Air Force Engineering University, Xi'an, 710038, China. lizhe08402@163.com.
Scientific reports
|May 6, 2024
概括
等离子体冰形状调节将连续冰转化为间歇冰,大大降低了机翼的飞行风险. 这项研究量化了降低飞行风险,显示了直翼和横翼的改善.
科学领域:
- 航空航天工程 航空航天工程
- 等离子体物理学的物理学
- 流体动力学 流体动力学
背景情况:
- 飞机机翼上不断积累的冰会降低空气动力学性能,增加飞行风险.
- 等离子体冰形状调节提供了一种低能量的方法,可以将冰转化为更安全的间歇形式.
研究的目的:
- 为了研究等离子体冰形状调节对机翼空气动力学和飞行安全的影响.
- 量化评估通过这种调节方法实现的飞行风险降低.
主要方法:
- 使用3D打印模型模拟NACA0012气翼上的调节后冰形状.
- 进行风洞实验以测量空气动力学参数.
- 采用可达到的集合方法来模拟飞行安全边界.
- 开发一种定量风险评估方法.
主要成果:
- 空气动力学特征受到调节冰宽度与翼弦长度的比率的显著影响.
- 与连续冰相比,调节的冰形状显示出更好的空气动力学性能.
- 定量飞行风险评估显示,直翼和横翼的风险水平 (2-4) 降低,调控比率为0.15.
结论:
- 等离子体冰形状调节有效地减轻了与冰积累相关的空气动力学惩罚.
- 该研究提供了一种定量方法来评估飞行风险降低,证明其对飞机安全的有效性.
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