An experimental investigation on low-velocity impact response and compression after impact of a stochastic, discontinuous prepreg tape composite

被引:26
作者
Kravchenko, Sergii G. [2 ]
Volle, Chris [1 ]
Kravchenko, Oleksandr G. [1 ]
机构
[1] Old Dominion Univ, Dept Mech & Aerosp Engn, Norfolk, VA 23529 USA
[2] Univ British Columbia, Dept Mat Engn, Composites Res Network, Vancouver, BC, Canada
关键词
Low-velocity impact; Impact behavior; Damage tolerance; Ultrasonic C-scan; Discontinuous fiber composite; INTRA-LAMINAR; DAMAGE; RESISTANCE; PERFORMANCE; STRENGTH; TENSILE;
D O I
10.1016/j.compositesa.2021.106524
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The present paper investigated the impact and compression after impact behavior of thin carbon fiber epoxy plates manufactured from prepreg platelet molding compound (PPMC) with two different discontinuous fiber length, 25.5 mm and 12.7 mm, and compared it with the behavior of continuous fiber quasi-isotropic composite laminate with a similar plate thickness. The results of dynamic testing showed that PPMC/12.7 mm exhibited larger amount of absorbed energy, which correlated with larger damage area measured by ultrasonic inspection. Micro-CT analysis showed that a discontinuous fiber composite developed significant amount of throughthickness damage. C-scan measured damage area correlated well with the compression after impact testing results, which indicated that longer fibers provide for better damage tolerance.
引用
收藏
页数:19
相关论文
共 59 条
[1]   An experimental investigation of the impact response of composite laminates [J].
Aktas, Mehmet ;
Atas, Cesim ;
Icten, Buelent Murat ;
Karakuzu, Ramazan .
COMPOSITE STRUCTURES, 2009, 87 (04) :307-313
[2]  
[Anonymous], 2007, APPL NEWS, P4
[3]   Experimental study of the impactor mass effect on the low velocity impact of carbon/epoxy woven laminates [J].
Artero-Guerrero, J. A. ;
Pernas-Sanchez, J. ;
Lopez-Puente, J. ;
Varas, D. .
COMPOSITE STRUCTURES, 2015, 133 :774-781
[4]   An overall view on impact response of woven fabric composite plates [J].
Atas, Cesim ;
Sayman, Onur .
COMPOSITE STRUCTURES, 2008, 82 (03) :336-345
[5]  
Aubry J., 2001, REINF PLAST, V45, P38, DOI DOI 10.1016/S0034-3617(01)80207-1
[6]   Low velocity impact tests of laminate glass-fiber-epoxy matrix composite material plates [J].
Belingardi, G ;
Vadori, R .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2002, 27 (02) :213-229
[7]   Observations of damage development from compression-after-impact experiments using ex situ micro-focus computed tomography [J].
Bull, D. J. ;
Spearing, S. M. ;
Sinclair, I. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2014, 97 :106-114
[8]   Effect of resin and fibre properties on impact and compression after impact performance of CFRP [J].
Cartié, DDR ;
Irving, PE .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2002, 33 (04) :483-493
[9]   Experimental investigation of the crush performance of prepreg platelet molding compound tubes [J].
Cutting, Rebecca A. ;
Rios-Tascon, Federico ;
Goodsell, Johnathan E. .
JOURNAL OF COMPOSITE MATERIALS, 2020, 54 (27) :4311-4324
[10]   Impact on composite structures [J].
Davies, GAO ;
Olsson, R .
AERONAUTICAL JOURNAL, 2004, 108 (1089) :541-563