正交层合板失效的参数化研究
Application ID: 143221
Laminated composite shells made from graphite–epoxy fiber-reinforced plies are widely used in many applications due to their high strength-to-weight ratio. Evaluating their structural integrity under applied loads is essential for ensuring reliable designs.
This example demonstrates failure analysis of a cross-ply laminate for different ply fiber angles. The model is subjected to multiple load cases and loaded to failure, considering in-plane stress states. Both classical and advanced failure criteria are described and compared.
案例中展示的此类问题通常可通过以下产品建模:
您可能需要以下相关模块才能创建并运行这个模型，包括：
- COMSOL Multiphysics® 和
- 复合材料模块 和
- 以下模块之一： MEMS 模块, 或 结构力学模块
建模所需的 COMSOL® 产品组合取决于多种因素，包括边界条件、材料属性、物理场接口及零件库，等等。不同模块可能具有相同的特定功能，详情可以查阅技术规格表，推荐您通过免费的试用许可证来确定满足您的建模需求的正确产品组合。如有任何疑问，欢迎咨询 COMSOL 销售和技术支持团队，我们会为您提供满意的答复。