在无人机喷过程中,下水和横风对空间原子化特征产生的反压:CFD分析和验证
Han Feng1, Pingfan Xu1,2, Shenghui Yang1
1College of Engineering, China Agricultural University, Beijing, China.
Pest management science
|November 2, 2023
概括
无人驾驶飞行器 (UAV) 的喷受风的影响. 增强下水可以改善喷雾均性,并抵消不利的横风影响,以提高应用性能.
科学领域:
- 农业工程 农业工程
- 流体动力学 流体动力学
- 航空航天工程 航空航天工程
背景情况:
- 无人驾驶飞行器 (UAV) 的喷受下水和横风的影响,改变了滴滴原子化特征.
- 了解这些空间原子化特征对于优化喷雾应用至关重要.
研究的目的:
- 调查旋转器速度和横风速度对无人机喷雾的空间原子化特征的影响.
- 为了澄清空气流,逆压和滴滴分布的基本机制.
主要方法:
- 计算流体动力学 (CFD) 模型是为了模拟空气流,逆压和原子化而开发的.
- 创建了一个验证平台,以实验验证CFD模型的结果.
主要成果:
- 负压原子化导致了更小的,凝聚在喷嘴附近的液滴,而正压产生了更大,更远的聚合液滴.
- 横风诱导的原子化分层和增加的喷雾漂移与速度.
- 转子速度的增加导致了更广泛的滴滴分布和更均的颗粒大小.
结论:
- 空间原子化与空气流和反压力动态密切相关.
- 下水改善滴滴分布的均性,抵消横风的负面影响.
- 优化下水是在现实应用中实现卓越喷性能的关键.
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