Damage Prediction of Integrated Composite T-Joint with Fixed Support Subjected to Low-Velocity Impact: An Experimental and Numerical Study

被引:0
作者
Rujian Zhu
Xiwu Xu
Chunjian Mao
机构
[1] Nanjing University of Aeronautics and Astronautics,The State Key Laboratory of Mechanics and Control of Mechanical Structures
来源
International Journal of Aeronautical and Space Sciences | 2019年 / 20卷
关键词
T-joint; Finite element model; Low-velocity impact; Impact damage;
D O I
暂无
中图分类号
学科分类号
摘要
A finite element model was established based on Hashin failure criteria and the progressive damage theory to predict the damage of integrated composite T-joint structures with fixed support subjected to low-velocity impact. The cohesive zone model was employed to simulate the delamination behaviors of adhesive in the finite element model. The fiber damage and matrix damage of each ply can be provided by the finite element model in details. The damage behaviors of composite T-joint structure subjected to different impact energies were compared using the finite element model. The numerical results showed that the impact caused an elliptical projected area with its major axis along the surface fiber direction. Besides, the in-plane damage dimension is proportional to the impact energy. It is obviously noted that the damage of the first ply is the most serious owing to the delamination between soleplate and fillet caused by the stretching of the L-ribs. A low-velocity impact experiment of composite T-joint was also conducted and the damage dimension was determined by the ultrasonic C-scan. Results showed that the shape and size of our experimental damage agreed well with the simulation results. Our finite element model can be used to effectively analyze the damage behaviors of the integrated composite T-joint subjected to low-velocity impact.
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页码:90 / 99
页数:9
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[1]  
Feng Y(2016)Investigation on tension-tension fatigue performances and reliability fatigue life of T700/MTM46 composite laminates Compos Struct 136 64-74
[2]  
Gao C(2014)Future structural stability design for composite space and airframe structures Thin Wall Struct 81 29-38
[3]  
He YT(2011)Effect of back pressure on impact and compression-after-impact characteristics of composites Compos Struct 93 944-951
[4]  
Degenhardt R(2014)Modelling the simulation of impact induced damage onset and evolution in composites Compos B 66 340-347
[5]  
Castro SGP(2008)Edge impact to composite laminates-experiments and simulations J Mater Sci 43 6661-6667
[6]  
Mariano AA(2008)Strain-based structural health monitoring of complex composite structures Struct Health Monit 7 203-213
[7]  
Zimmerman R(2013)Experimental study on barely visible impact damage and visible impact damage for repair of small aircraft composite structure Aerosp Sci Technol 29 363-372
[8]  
Khakimova R(2012)Numerical simulation of the failure of composite T joints with defects Acta Aeronaut Astronaut Sin 33 287-296
[9]  
Kling A(2003)Influence of the laminate thickness in low velocity impact behavior of composite materials plate Compos Struct 61 27-38
[10]  
Mandar DK(2002)Effect of resin and fiber properties on impact and compression after impact performance of CFRP Compos Part A 33 483-493