由于空气动力学负载,低音飞机机翼的最佳设计
Ibtisam J Ismeal1, Mehmet Bakirci1, Muhsin J Jweeg2
1Karabuk University, Karabuk, Türkiye.
TheScientificWorldJournal
|January 25, 2024
概括
这项研究优化了L-39 A/C飞机机翼设计,以使用蜂结构来实现高强度和低重量. 与传统的翅膀结构相比,蜂设计提供了优越的硬度与重量比率.
科学领域:
- 航空航天工程 航空航天工程
- 结构分析 结构分析
- 计算流体动力学的流体动力学.
背景情况:
- 飞机机翼故障是航空事故的重要原因之一.
- 翅膀对于产生升力和飞行稳定性至关重要.
- 优化机翼设计的强度和重量对于飞机的安全和性能至关重要.
研究的目的:
- 为了确定L-39 A/C飞机机翼的最佳结构设计参数.
- 通过先进的结构建模来实现高强度和最小重量.
- 为了评估蜂巢翼结构的性能.
主要方法:
- 使用SOLIDWORKS 2020进行翼模型 (蜂结构) 的数值模拟.
- 使用FLUENT 2022 R1.1.进行空气动力学压力预测.
- 使用ANSYS软件进行应力和变形分析.
- 与传统的翅膀设计 (肋骨和绳索) 的比较.
主要成果:
- 蜂巢翼模型显示出显著的结构完整性.
- 可以准确预测空气动力学压力分布.
- 在空气动力学负荷下量化了应力和变形.
- 蜂巢设计表现出高的硬度与重量比.
结论:
- 蜂巢结构设计是飞机机翼的可靠和可接受的方法.
- 与传统方法相比,优化的设计提供了优越的硬度与重量比率.
- 这项研究有助于提高飞机机翼的安全性和效率.
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