在短暂的空气动力学加热上对高超音速复合机翼的热模分析
Kangjie Wang1, Junli Wang2,3, Zhiyuan Liu1
1School of Mechanical Engineering, Shaanxi University of Technology, Hanzhong, 723001, Shaanxi, China.
Scientific reports
|May 14, 2024
概括
本研究分析了在空气动力加热下复合机翼中的高超音速空热结构合. 温度变化显著影响自然频率,特别是由于早期材料的特性变化.
科学领域:
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
- 计算流体动力学的流体动力学.
背景情况:
- 超音速飞行会产生极端的空气动力学加热,对飞机材料构成挑战.
- 了解气热结构合对于设计高速飞机至关重要.
- 复合材料作为热保护系统具有潜力,但需要进行彻底的分析.
研究的目的:
- 开发一种数值方法来分析复合机翼中的高超音速气热结构合.
- 研究过渡温度分布及其对热模特特征的影响.
- 确定影响复合机翼在空气动力加热下热模态行为的因素.
主要方法:
- 采用纳维埃-斯托克斯方程和富里埃导热定律进行半隐性时间域数值分析.
- 利用有限元法计算不同时间点的热模性质.
- 分析了不同翼区域温度的时间变化以及影响热模态行为的因素.
主要成果:
- 复合机翼的前边首先达到热平衡,其次是后边;腹板显示较慢的热反应.
- 温度上升显著影响更高阶的振动模式.
- 在早期加热阶段物质性质的变化是导致自然频率快速下降的主要因素.
结论:
- 复合材料是有效的飞机热保护.
- 空气动力加热会影响机翼的热模式特性,早期加热阶段主要由材料性质的变化所主导.
- 随着加热的进展,热应力变得越来越有影响力,导致自然频率的减缓甚至增加.
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