通过先进的计算模拟,设计,动力学和开发升级的可倾斜翼相关的四旋翼,并采用了自下而上的方法
Haribalan Saravana Mohan1, Karthikeyan Murugaraj1, Senthil Kumar Solaiappan1
1Department of Aeronautical Engineering, Kumaraguru College of Technology, Coimbatore, Tamil Nadu, India.
Scientific reports
|April 8, 2025
概括
这项研究介绍了一种混合无人飞行器 (HUAV),其机翼形臂和倾斜转子/翼设计可提高耐力和稳定性. 计算流体动力学和结构分析证实了它的效率和适用于恶劣环境的适用性.
科学领域:
- 航空航天工程 航空航天工程
- 计算流体动力学的流体动力学.
- 结构分析 结构分析
背景情况:
- 传统的无人驾驶飞行器 (UAV) 面临着耐久性限制.
- 混合动力设计为提高性能和多功能性提供了潜力.
- 降低空气动力阻力对于提高无人机耐力至关重要.
研究的目的:
- 设计和分析混合无人飞行器 (HUAV),以提高耐久性和稳定性.
- 为了研究一种新的倾斜翼和倾斜旋转机配置的性能.
- 为了评估气形状横截面臂对阻力减轻的影响.
主要方法:
- 计算流体动力学 (CFD) 用于流体流动分析.
- 流体结构相互作用 (FSI) 用于结构和空气动力学负载分析.
- 数学建模和控制器设计,以确保稳定性和机动性.
主要成果:
- 空翼横截面臂显著减少阻力,增强耐力.
- 混合动力配置在恶劣环境中表现出稳定性.
- GY-70-CFRP复合材料被确定为翼和螺旋结构的最佳材料.
结论:
- 拟议的HUAV设计提供了更好的空气动力学效率和耐久性.
- 倾斜翼和倾斜旋翼概念的整合提高了机动性和稳定性.
- 该研究通过CFD,FSI,分析和实验方法验证设计.
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