Monitoring mode II fracture behaviour of composite laminates using embedded fiber-optic sensors

2007 ◽  
Vol 38 (4) ◽  
pp. 488-497 ◽  
Author(s):  
Hang-Yin Ling ◽  
Kin-Tak Lau ◽  
Zhongqing Su ◽  
Eric Tsun-Tat Wong
Keyword(s):  
Composite Laminates ◽  
Fiber Optic ◽  
Fracture Behaviour ◽  
Fiber Optic Sensors ◽  
Mode Ii ◽  
Mode Ii Fracture

Interlaminar Fracture Toughness of Composite Laminate with Splicing Plies

2011 ◽  
Vol 194-196 ◽  
pp. 1697-1702
Author(s):  
Li Liang ◽  
Pu Rong Jia ◽  
Gui Qiong Jiao
Keyword(s):  
Fracture Toughness ◽  
Composite Laminates ◽  
Tensile Testing ◽  
Mode Ii ◽  
Interlaminar Fracture Toughness ◽  
Fiber Reinforced ◽  
Interlaminar Fracture ◽  
Mode Ii Fracture ◽  
Mode Ii Fracture Toughness ◽  
Delamination Failure

Delamination is one of the important damage modes in the fiber-reinforced composite laminates. The interlaminar fracture toughness is the key parameter in delamination failure analysis of composites. The stress analysis by a finite element modeling has shown that the shear stress is very large near the ply splicing area. So the delamination failure is mainly dependent on the mode II fracture toughness. A new way of loading in tensile testing is proposed for the measurement of mode II fracture toughness. Specific specimen with splicing plies has been designed and used for the experiment. Testing study on the carbon-fiber-reinforced laminate with ply splicing was performed. Steady crack propagation has been seen by the tensile testing of the specimen. Mode II fracture toughness GIIC of the laminate has been determined by the experiment data analysis. The experiment and numerical analysis shows that the tensile testing for the measurement of mode II interlaminar fracture toughness is feasible.

Cohesive zone modeling of the autoclave pressure effect on the delamination behavior of composite laminates

2018 ◽  
Vol 37 (24) ◽  
pp. 1468-1480
Author(s):  
Tengfei Chang ◽  
Lihua Zhan ◽  
Wei Tan ◽  
Xintong Wu
Keyword(s):  
Fracture Toughness ◽  
Cohesive Zone ◽  
Composite Laminates ◽  
Cohesive Zone Model ◽  
Cohesive Strength ◽  
Mode Ii ◽  
Zone Model ◽  
Mode Ii Fracture ◽  
Mode Ii Fracture Toughness ◽  
Delamination Behavior

Current manufacturing processes using resin transfer molding or low-pressure prepreg curing may result in different defects and interfacial properties. The effect of autoclave pressure on the delamination behavior of T800/X850 composite laminates is explored. Cohesive zone model was used to model the delamination of unidirectional composite laminates under short-beam bending. Composites with various interlaminar properties were manufactured using autoclave under cure pressure from 0 MPa to 0.6 MPa. Cohesive zone model was validated using the material parameters of the composite cured under 0.6 MPa. The effect of cohesive zone model parameters including cohesive strength, mode I fracture toughness ([Formula: see text]), and mode II fracture toughness ([Formula: see text]) on the delamination behavior and load–displacement response was investigated. Parametric study shows that interlaminar cohesive strength and mode II fracture toughness dominated the initiation of yield and post-yield region, respectively. The correlation between autoclave pressure and mode II fracture toughness was predicted, which is mainly affected by void content.

Cure monitoring of composite laminates using fiber optic sensors

2002 ◽  
Vol 11 (2) ◽  
pp. 279-287 ◽  
Author(s):  
Hyun-Kyu Kang ◽  
Dong-Hoon Kang ◽  
Hyung-Joon Bang ◽  
Chang-Sun Hong ◽  
Chun-Gon Kim
Keyword(s):  
Composite Laminates ◽  
Fiber Optic ◽  
Fiber Optic Sensors ◽  
Cure Monitoring
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