Numerical Analysis for Determination of the J Integral and Crack Opening Displacement in the Cracked Aluminum Plates Repaired with FML Composite Patches

Gholamhassan Payganeh; Faramarz Ashenai Ghasemi; Ali Pourkamali Anaraki; Ahmad Fallah Rahmatabadi

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Numerical Analysis for Determination of the J Integral and Crack Opening Displacement in the Cracked Aluminum Plates Repaired with FML Composite Patches

机译：用FML复合修补剂修复裂纹铝板J积分和裂纹开口位移确定的数值分析。

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Fiber Metal Laminates (FMLs) are widely used in aerospace industries nowadays. In this study, numerical investigations of adhesively bonded FML composite patch repairs of cracked aluminum panels is reported. Pre-cracked 3035 Aluminum panels of 179x76x1.5

机译：如今，纤维金属层压板（FML）广泛用于航空航天工业。在这项研究中，报道了破裂的铝面板的粘合FML复合材料补片修复的数值研究。预开裂的179x76x1.5的3035铝板

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《Journal of Applied Sciences》 |2012年第21期|共7页
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Gholamhassan Payganeh; Faramarz Ashenai Ghasemi; Ali Pourkamali Anaraki; Ahmad Fallah Rahmatabadi;
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1. Numerical Analysis for Determination of the J Integral and Crack Opening Displacement in the Cracked Aluminum Plates Repaired with FML Composite Patches [J] . Gholamhassan Payganeh, Faramarz Ashenai Ghasemi, Ali Pourkamali Anaraki, Journal of Applied Sciences . 2012,第21期

机译：用FML复合修补剂修复裂纹铝板J积分和裂纹开口位移确定的数值分析。
2. Numerical analysis for the determination of the stress intensity factors and crack opening displacements in plates repaired with single and double composite patches [J] . Madani K, Touzain S, Feaugas X, Computational Materials Science . 2008,第3期

机译：确定单层和双层复合材料修补板的应力强度因子和开裂位移的数值分析
3. A Study on the Charpy Impact Response of the Cracked Aluminum Plates Repaired with FML Composite Patches [J] . Faramarz Ashenai Ghasemi, Lotfali Mozafari Vanani, Ali Pourkamali Anaraki Journal of Failure Analysis and Prevention . 2016,第4期

机译：FML复合材料修补铝板裂纹的夏比冲击响应研究
4. Impact Behavior of Cracked Plate Repaired With Composite and FML Patches [C] . M. Sadeghinia, S. M. R. Khalili, R. Ghadjar International Conference on Multifunctional Materials and Structures . 2008

机译：用复合材料和FML贴片修复破裂板的影响行为
5. A Numerical and Experimental Study of Adhesively Bonded Repairs of Aluminum Fuselage Structures Using Aluminum and Composite Patches [D] . Chadha, Reewanshu 2018

机译：用铝和复合材料修补铝制机身结构的数值和实验研究
6. Fatigue Life Improvement of Cracked Aluminum 6061-T6 Plates Repaired by Composite Patches [O] . Armin Yousefi, Saman Jolaiy, Reza Hedayati, 2021

机译：复合贴片修复裂纹铝6061-T6板的疲劳寿命改进
7. Numerical analysis of surface cracks repaired with single and double patches of composites [O] . Inés Iváñez, Matías Braun 2017

机译：用单贴复合材料修复表面裂纹的数值分析
8. Thickness Effects on a Cracked Aluminum Plate with Composite Patch Repair [R] . Schubbe, J. J. 1997

机译：复合膜修补对裂纹铝板的厚度影响

Numerical Analysis for Determination of the J Integral and Crack Opening Displacement in the Cracked Aluminum Plates Repaired with FML Composite Patches

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