一种层合板受冲击时的分析方法

By enhancing the Lagrange multiplier and elliptic transformation method, and combining finite deformation theory and the principle of virtual work, the complexity and computational difficulty in damage analysis of fiber-reinforced composite laminates are solved, achieving accurate interfacial contact and efficient damage prediction.

CN116644626BActive Publication Date: 2026-07-17WUHAN UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
WUHAN UNIV
Filing Date
2023-04-19
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing fiber-reinforced composite laminates have complex damage and failure modes, traditional failure criteria lack universality, and calculation methods are prone to ill-conditioned calculations and increased computational load.

Method used

A method based on enhanced Lagrange multipliers and elliptic transformation is adopted, and interface contact analysis is performed through finite deformation theory and the principle of virtual work. Combined with matrix failure criteria and layered growth criteria, accurate constraints and efficient calculations are achieved.

Benefits of technology

It achieves precise interface contact constraints when laminates are subjected to impact, avoiding ill-conditioned calculations and a significant increase in computational load, thus improving analysis efficiency and accuracy.

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Abstract

本申请公开了一种层合板受冲击时的分析方法。本分析方法基于增强拉格朗日方法实现界面接触分析,不仅实现精确的接触约束,还避免了计算量的大幅增加。另外通过迭代方法得到拉格朗日乘子,使得罚参数的选取更加容易,且不会引起病态计算的现象。在损伤预测分析模型中,通过基体开裂准则和分层增长准则分别预测基体裂纹与分层损伤的发生。为简化应变能释放率的计算,本发明提出一种改进的椭圆变换方法。该方法基于标准的椭圆变换,引入缩放因子来“拉伸”网格,使得分层前沿与附近的网格线保持很好的正交性。本发明提出的数值分析方法简便、计算效率高,有利于理解包含基体裂纹与分层增长的复合材料层合板的损伤力学。
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