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Material parameter modeling and solution technique using birth–death element for notched metallic panel repaired with bonded composite patch

机译：利用粘合复合贴片修复缺口金属板的生死元件材料参数建模与求解技术

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Tong Lei; Li Shiqiu; Xiong Junjiang;
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年度 2014
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1. Material parameter modeling and solution technique using birth-death element for notched metallic panel repaired with bonded composite patch [J] . Tong Lei, Li Shiqiu, Xiong Junjiang 中国航空学报（英文版） . 2014,第002期

机译：结合复合补片修复的缺口金属面板使用生死元素的材料参数建模和求解技术
2. Integrated experimental screening of bonded composites patch repair schemes to notched aluminum-alloy panels based on static and fatigue strength concepts [J] . J.J. Xiong, R.A. Shenoi Composite Structures . 2008,第3期

机译：基于静态和疲劳强度概念的粘结复合材料修补程序对缺口铝合金面板的集成实验筛选
3. Modeling of cracked thick metallic structure with bonded composite patch repair using three-layer technique [J] . J.J. Schubbe, S. Mall Composite Structures . 1999,第3期

机译：三层技术结合复合材料修补修复裂纹厚金属结构
4. Effects of patch geometrical parameters on mechanical properties of damaged metallic structure repaired with adhesively bonded composite patch [C] . Zhou Kai, Zhang Ding, Wang Haidong International Conference on Mechanical Structures and Smart Materials . 2014

机译：贴片几何参数对粘接复合贴剂修复损坏金属结构力学性能的影响
5. A comparison of patch and fully encircled bonded composite repairs in pressure vessels with through-wall defects. [D] . Theisen, Stephen A. 2017

机译：具有通孔缺陷的压力容器中修补和完全环绕的粘结复合材料修复的比较。
6. Structural Materials: Identification of the Constitutive Models and Assessment of the Material Response in Structural Elements Strengthened with Externally-Bonded Composite Material [O] . Todor Zhelyazov 2020

机译：结构材料：本构模型的识别和外部结合复合材料加强的结构元件中材料响应的评估
7. Material parameter modeling and solution technique using birth–death element for notched metallic panel repaired with bonded composite patch [O] . Tong Lei, Li Shiqiu, Xiong Junjiang 2014

机译：用生死元素对带粘结复合材料修补件的缺口金属面板进行材料参数建模和求解技术
8. Modeling and Lowering Residual Stresses in Bonded Composite Patch Repairs of Metallic Aircraft Stuctures [R] . Sun, C. T. , Caruthersw, M. 2001

机译：金属飞机结构粘结复合补片修复中的残余应力建模与降低

Material parameter modeling and solution technique using birth–death element for notched metallic panel repaired with bonded composite patch

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