scholarly journals Multiscale approach for identification of transverse isotropic carbon fibre properties and prediction of woven elastic properties using ultrasonic identification

2018 ◽  
Vol 168 ◽  
pp. 160-169 ◽  
Author(s):  
R.D.B. Sevenois ◽  
D. Garoz ◽  
E. Verboven ◽  
S.W.F. Spronk ◽  
F.A. Gilabert ◽  
...  
2020 ◽  
Vol 8 (1) ◽  
Author(s):  
Jyotikalpa Bora ◽  
Sushen Kirtania

Abstract A comparative study of elastic properties and mode I fracture energy has been presented between conventional carbon fibre (CF)/epoxy and advanced carbon nanotube (CNT)/epoxy laminated composite materials. The volume fraction of CNT fibres has been considered as 15%, 30%, and 60% whereas; the volume fraction of CF has been kept constant at 60%. Three stacking sequences of the laminates viz.[0/0/0/0], [0/90/0/90] and [0/30/–30/90] have been considered in the present analysis. Periodic microstructure model has been used to calculate the elastic properties of the laminated composites. It has been observed analytically that the addition of only 15% CNT in epoxy will give almost the same value of longitudinal Young’s modulus as compared to the addition of 60% CF in epoxy. Finite element (FE) analysis of double cantilever beam specimens made from laminated composite has also been performed. It has been observed from FE analysis that the addition of 15% CNT in epoxy will also give almost the same value of mode I fracture energy as compared to the addition of 60% CF in epoxy. The value of mode I fracture energy for [0/0/0/0] laminated composite is two times higher than the other two types of laminated composites.


Author(s):  
P. Rupnowski ◽  
M. Gentz ◽  
J. K. Sutter ◽  
M. Kumosa

In this work, a methodology has been presented for the evaluation of stiffness properties and temperature–dependent coefficients of thermal expansion of continuous fibres from the macroscopic properties of either unidirectional or woven composites. The methodology was used to determine the stiffness and thermal properties of T650–35 graphite fibres from the macroscopic input data of unidirectional and woven composites based on the same fibres embedded in a PMR–15 polyimide matrix. In the first part of the analysis, the fibre properties were determined directly from the unidirectional composite macro data using the inversed Eshelby–Mori–Tanaka approach. Subsequently, certain fibre properties were additionally evaluated indirectly from the woven composite, using the finite–element method and the concept of a representative unit cell. It has been shown that the temperature–dependent coefficients of thermal expansion of the fibres can be estimated from the unidirectional composite macro data with significantly smaller errors than in the case of the elastic properties. It has also been shown that the errors in the evaluation of the elastic properties of the fibres from the macro unidirectional composite data could be significantly reduced if the fibres were placed in a stiff matrix material: much stiffer than the polyimide resin. The longitudinal and transverse coefficients of thermal expansions and the shear modulus of the T650–35 fibres determined from the unidirectional composite analysis were successfully verified by investigating the woven composite.


2000 ◽  
Vol 9 (6) ◽  
pp. 096369350000900 ◽  
Author(s):  
Q. Yuan ◽  
J. Karger-Kocsis ◽  
L. Ye

Cross-ply and quasi-isotropic carbon fibre reinforced epoxy (CF/EP) laminates were toughened by addition of interleaves, which consisted of either a modified epoxy resin or random PET mat embedded in a modified epoxy resin. Impact and multiple impact performances of the laminates were studied using an instrumented falling weight impact tester. A simple model was used to correlate the performance of the laminates under multiple impact.


2015 ◽  
Vol 23 (7) ◽  
pp. 475-482 ◽  
Author(s):  
Hossein Rahmani ◽  
S. Heydar Mahmoudi Najaf ◽  
Alireza Ashori ◽  
Mahdi Golriz

1974 ◽  
Vol 22 (1) ◽  
pp. 45-48 ◽  
Author(s):  
J. V. Sharp ◽  
S. G. Burnay

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