为陶纤维绝缘建立和应用弹性-塑料损伤构成模型
Yiming Wang1, Yesheng Zhong1, Yining Huang2
1Center for Composite Materials and Structures, Harbin Institute of Technology, Harbin 150080, China.
Materials (Basel, Switzerland)
|January 8, 2025
概括
一个新的弹性塑料损伤模型准确地预测了陶纤维绝缘 (CFIT) 的机械行为. 这种经过验证的模型增强了对CFIT在苛刻的航空航天应用中的表现的理解.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 陶纤维绝缘 (CFIT) 对于飞机的热保护系统至关重要.
- CFIT是多孔的,3D网络材料,具有复杂的机械行为.
- 现有的实验和模拟方法难以准确地捕捉CFIT机械反应.
研究的目的:
- 为CFITs开发和验证可靠的弹性-塑性损伤构成模型.
- 准确预测CFIT在各种工作条件下的复杂机械行为.
- 改进飞机热保护系统的设计和安全性.
主要方法:
- 为CFITs建立了一个弹性-塑料损伤构成模型.
- 该模型结合了哈希恩标准和一个修改后的收益率规则与损害因子.
- 该模型作为用户材料子程序 (UAMT) 在ABAQUS中实现.
主要成果:
- 模拟曲线与实验数据密切匹配,压力-应变关系得到了准确的描述.
- 该模型显示了预测准确度,压缩,张力和剪切的误差小于18%.
- 通过缩进实验进行验证,显示最大负载深度在12%的误差范围内保持一致.
结论:
- 开发的弹性-塑料损伤构成模型可靠地预测CFIT机械行为.
- 该模型为分析复杂的航空航天环境中的CFIT性能提供了有价值的工具.
- 该研究有助于提高飞机热保护系统的安全性和效率.
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