In situ damage characterization of CFRP under compression using high-speed optical, infrared and synchrotron X-ray phase-contrast imaging

被引:10
作者
Pournoori, Nazanin [1 ]
Soarea, Guilherme Correa [1 ]
Lukic, Bratislav [2 ]
Isakov, Matti [1 ]
Belone, Maria Clara Lessa [1 ]
Hokka, Mikko [1 ]
Kanerva, Mikko [1 ]
机构
[1] Tampere Univ, Fac Engn & Nat Sci, Engn Mat Sci, POB 33014, Tampere, Finland
[2] European Synchrotron Radiat Facil, F-38043 Grenoble 9, France
关键词
Carbon fiber-reinforced polymer composites; Adiabatic heating; High strain rate; Compressive damage; FIBER-REINFORCED POLYMERS; STRAIN-RATE; MECHANICAL-PROPERTIES; COMPOSITES; BEHAVIOR; IMPACT;
D O I
10.1016/j.compositesa.2023.107766
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The strain rate dependency and failure modes of carbon fiber reinforced plastic (CFRP) laminate were investigated under out-of-plane compressive loading. Simultaneous high-speed optical and infrared imaging were used to measure full-field deformation and temperature in the dynamically loaded specimens. The damage initiation and propagation inside the CFRP laminates at high strain rates were characterized using in-situ ultra-fast synchrotron X-ray phase contrast imaging (XPCI). The visually observed damage onset occurs at the strain value of 4.2 +/- 0.6% as a transverse shear fracture at the free edge of specimens. The local temperature increases significantly to 185 degrees C due to damage initiation at high strain rates, while at low strain rates the temperature rise occurs after the final shear band forms. The XPCI and post-failure analysis provide an integrated perspective on the formation of a diagonal shear crack and disintegration of the specimen into two pieces with the fracture of plies in the in-plane transverse direction. Scanning electron microscopic (SEM) study was integrated with XPCI results to append the time scale for the post-mortem failure pattern as well as the length scale for microcracks and filament-level failure.
引用
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页数:11
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