超轻细胞三明治板的三维振动理论,这些板受到直线变化的平面内分布负荷的影响
Fei-Hao Li1,2, Bin Han3, Ai-Hua Zhang1
1The Institute of Xi'an Aerospace Solid Propulsion Technology, Xi'an 710025, China.
Materials (Basel, Switzerland)
|June 10, 2023
概括
重力和加速显著影响薄型航空航天结构. 这项研究开发了超轻型三明治板的振动理论,发现三角波纹芯提供了最高的基本频率,这对航空航天安全至关重要.
科学领域:
- 固体力学 固体力学是什么
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
背景情况:
- 航空航天领域的薄结构元素容易受到重力和加速力的影响.
- 了解这些结构在这种负载下的机械行为对于安全和性能至关重要.
研究的目的:
- 开发一个3D振动理论超轻的细胞核心的三明治板在线性变化的在平面负载下.
- 研究核心类型和几何参数对这些板块基本频率的影响.
- 用3D有限元模拟来验证理论模型.
主要方法:
- 采用了一种齐克扎克式移位模型来建立3D振动理论.
- 该理论解释了由于面板剪切而导致的横截面旋转角度.
- 为了验证,进行了三维有限元模拟.
主要成果:
- 该研究量化了不同核心类型 (金属泡,波纹板,蜂) 对基本频率的影响.
- 三角波纹三明治板在各种边界条件中表现出最高的基本频率.
- 发现平面内分布的负荷对所有被考虑的三明治板类型的基本频率和模态形状产生了显著的改变.
结论:
- 经过验证的理论为分析超轻型三明治板在重力/加速下的动态行为提供了强大的工具.
- 三角波纹芯是最大化航空航天应用中的基本频率的最佳选择.
- 设计考虑必须包括飞机内负荷对结构动态的影响.
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