实验和数值调查在一个三体船的空中醒觉,几何学修改
Karim Akbari Vakilabadi1, Hamid Reza Ghafari2, Hassan Ghassemi2
1Department of Mechanical Engineering, Imam Khomeini Naval University, Noshahr, Iran.
Heliyon
|November 3, 2023
概括
研究人员研究了三船飞行甲板的几何结构,以减少空气压力差异. 优化设计,采用形边缘,显著降低了压力变化,改善了直升机在动荡条件下降落的安全性.
科学领域:
- 海军建筑 海军建筑
- 空气动力学 在空气动力学.
- 流体动力学 流体动力学
背景情况:
- 直升机与船舶的互动对操控和性能构成挑战,特别是在流中.
- 特里马兰飞行甲板设计对于安全的直升机操作至关重要.
- 了解飞行甲板上的空气流对于减轻空气动力学风险至关重要.
研究的目的:
- 为了研究三体船飞行甲板几何形状对空气压力分布的影响.
- 评估不同的顶部结构设计,以尽量减少压力差异.
- 为优化直升机操作飞行甲板配置提供见解.
主要方法:
- 利用计算流体动力学 (CFD) 进行空气压力分析.
- 使用粒子图像速度计 (PIV) 进行实验验证.
- 在不同的风速和雷诺兹数下评估各种几何形状.
主要成果:
- 与基本设计 (A) 相比,确定了特定的几何形状 (C和F),压力差异较小.
- 在45度和30度的边被证明是有效的,以尽量减少压力变化.
- 雷诺德数对压力的影响可以忽略不计,除了最高值 (Re=50e6) 和特定位置 (x/L=0.5) 之外.
结论:
- 飞行甲板的几何结构显著影响空气压力,影响空气动力学相互作用.
- 经过优化后的三轮船飞行甲板设计,并配有特定的机,可以提高安全性.
- 该研究提供了一种经过验证的方法,用于对船舶飞行甲板的空气动力学分析.
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