Modeling Flexural Failure in Carbon-Fiber-Reinforced Polymer Composites

被引:6
作者
Burgani, Thiago de Sousa [1 ]
Alaie, Seyedhamidreza [2 ]
Tehrani, Mehran [1 ]
机构
[1] Univ Texas Austin, Walker Dept Mech Engn, Austin, TX 78712 USA
[2] New Mexico State Univ, Dept Mech & Aerosp Engn, Las Cruces, NM 88003 USA
关键词
carbon fiber; fiber-reinforced polymer composite; flexural strength; modeling; failure mode; finite-element analysis;
D O I
10.3390/jcs6020033
中图分类号
TB33 [复合材料];
学科分类号
摘要
Flexural testing provides a rapid and straightforward assessment of fiber-reinforced composites' performance. In many high-strength composites, flexural strength is higher than compressive strength. A finite-element model was developed to better understand this improvement in load-bearing capability and to predict the flexural strength of three different carbon-fiber-reinforced polymer composite systems. The model is validated against publicly available experimental data and verified using theory. Different failure criteria are evaluated with respect to their ability to predict the strength of composites under flexural loading. The Tsai-Wu criterion best explains the experimental data. An expansion in compressive stress limit for all three systems was observed and is explained by the compression from the loading roller and Poisson's effects.
引用
收藏
页数:10
相关论文
共 16 条
[1]  
[Anonymous], 2015, D7264D7264M07 ASTM
[2]  
Budynas R.G., 2020, SHIGLEYS MECH ENG DE, V11th, P119
[3]  
Daniel I, 2006, Engineering mechanics of composite materials
[4]   Flexural performance of sandwich panels comprising polyurethane core and GFRP skins and ribs of various configurations [J].
Fam, Amir ;
Sharaf, Tarek .
COMPOSITE STRUCTURES, 2010, 92 (12) :2927-2935
[5]  
Favaloro M., THERMOPLASTIC COMPOS
[6]  
Francis S., 2019, THERMOPLASTIC COMPOS
[7]  
Gardiner G., 2021, INTEGRATING ANTENNAS
[8]  
Lian E., 2021, NATL I AVIAT RES
[9]  
Marlett K., 2011, NATL I AVIAT RES
[10]  
N.A. ANSYS Inc, 2021, FAIL CRIT REINF MAT