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复合材料制造的喷气式飞行器空中目标空气动力学性能的实验测试和数值分析
Michał Frant1, Łukasz Kiszkowiak1, Maciej Majcher1
1Faculty of Mechatronics, Armament and Aerospace, Military University of Technology, Kaliskiego 2 St., 00-908 Warsaw, Poland.
Materials (Basel, Switzerland)
|July 27, 2024
概括
本研究详细介绍了用于新型喷气式空中目标的空气动力学测试和计算流体动力学分析. 该研究验证了飞机设计的方法,从而产生了该系统.
科学领域:
- 航空航天工程 航空航天工程
- 流体动力学 流体动力学
- 计算力学 计算力学 计算力学
背景情况:
- 飞机的结构设计和材料选择取决于任务要求和施加的负载.
- 了解空气动力学负载对于设计轻量级,硬和耐用飞机结构至关重要.
研究的目的:
- 介绍一种新型喷气式空中目标的空气动力学实验和数值分析结果.
- 验证空气动力学分析的综合实验和计算流体动力学 (CFD) 方法的有效性.
主要方法:
- 实验性空气动力学测试在低速风洞中进行,跨越各种攻击角度和侧滑坡.
- 使用基于有限体积方法 (FVM) 的专用软件进行数值分析,用于解决部分微分方程.
- 将风洞数据与CFD模拟结果进行比较和整合.
主要成果:
- 分析了空气动力学力和时刻元件,并将其作为攻击角度和侧滑的函数呈现出来.
- 实现了空中目标周围空气流模式的定性可视化.
- 实验和数值结果证实了所采用的方法的充分性.
结论:
- 综合空气动力学分析方法为飞机设计提供可靠的数据.
- 新设计的空中目标系统成功通过了资格测试,并获得了型号认证.
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