分层尺寸和深度对硬化航空航天复合板压缩疲劳行为的影响
Angela Russo1, Rossana Castaldo1, Concetta Palumbo1
1Department of Engineering, University of Campania Luigi Vanvitelli, Via Roma 29, 81030 Aversa, Italy.
本研究分析了分层尺寸和深度如何影响压缩疲劳下的复合航空板. 了解这些因素对于提高航空航天结构安全性和可靠性至关重要.
科学领域:
- 航空航天工程 航空航天工程
- 材料科学 材料科学 材料科学
- 结构完整性 结构完整性
背景情况:
- 分层是复合材料航空航天结构的关键故障模式.
- 在压缩下评估疲劳行为对于结构可靠性至关重要.
研究的目的:
- 为了对分层复合航空板的疲劳行为进行灵敏度分析.
- 评估分层尺寸和深度对面板生命周期和结构完整性的影响.
主要方法:
- 使用独立于网格和负载步骤的数值程序进行可靠的分析.
- 研究了各种分层尺寸和位置,以模拟各种损坏场景.
主要成果:
- 量化了分层参数对疲劳寿命和结构性能的影响.
- 确定了在压缩疲劳期间影响面板完整性的关键分层场景.
结论:
- 灵敏度分析为设计更安全,更可靠的航空航天结构提供了关键的见解.
- 强大的数值程序对于精确的复合板分层影响评估至关重要.
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