对航空航天结构的多层蜂复合材料有限元素分析的比较研究
Miruna Ciolca1, Raul Cormos1,2, Catalin Andrei Neagoe1,3
1Department of Strength of Materials, National University of Science and Technology POLITEHNICA Bucharest, Splaiul Independentei 313, 060042 Bucharest, Romania.
Materials (Basel, Switzerland)
|May 7, 2025
概括
本研究介绍了两种有限元素模型,用于在压缩下分析新的多层蜂复合材料. 一个详细的模型提供了高精度,而一个简化的模型实现了80%的复杂性更少,可接受的结果用于航空航天应用.
科学领域:
- 机械工程 机械工程
- 材料科学 材料科学 材料科学
- 航空航天工程 航空航天工程
背景情况:
- 蜂复合材料在重量敏感的应用中至关重要,如航空航天.
- 这些材料旨在承受显著的压力负荷.
- 新的多层蜂复合材料与浸的纸芯呈现独特的分析挑战.
研究的目的:
- 为新型多层蜂复合材料提供两个有限元素模型 (FEM) 分析.
- 为了比较详细的本地分析模型与简化的全球分析模型的精度和效率.
- 通过实验性比较验证模型并提出实际应用.
主要方法:
- 开发详细的FEM用于蜂复合材料的局部变形分析.
- 开发用于全球分析的简化FEM,实现80%的复杂性降低.
- 两种模型的比较分析,随后进行实验验证.
主要成果:
- 详细的模型提供了高度精确的变形估计.
- 简化的模型提供了显著降低复杂性 (80%),同时产生可接受的结果.
- 实验验证表明与拟议的建模方法相一致.
结论:
- 详细和简化的FEM方法都适用于分析多层蜂复合材料.
- 简化模型在计算效率和结果准确性之间提供了实际的平衡.
- 这项研究表明了这些先进的复合材料在航空航天工程中的潜力.
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