TY - JOUR
T1 - Puck's Criterion for the tensile response of composite laminates
T2 - A numerical approach
AU - Pai, Anand
AU - Suri, Rishabh
AU - Bhave, Aniket Kunal
AU - Verma, Pranay
AU - N H, Padmaraj
N1 - Publisher Copyright:
© 2022
PY - 2023/1
Y1 - 2023/1
N2 - Material designers have extensively analyzed, utilizing failure theories, the dependability and service response of composite materials for their intended uses. To increase the precision and accuracy of performance prediction, failure theories have undergone numerous revisions. The current study uses the finite element method to predict the tensile response while also using Puck's failure criterion and the damage evolution law to composite laminates. Five non-hybrid sequences made of paperboard, ultra-high molecular weight polyethylene (UHMWPE), glass fibre, aramid fibre, and carbon fibre have been put through experimental investigation of tensile and three-point bending. The numerical analysis has been carried out using the Material Designer, ACP® and Structural Analysis modules of ANSYS® finite element software. The experimental results have been compared with the numerical results, to arrive at the set of empirical constants for the different materials.
AB - Material designers have extensively analyzed, utilizing failure theories, the dependability and service response of composite materials for their intended uses. To increase the precision and accuracy of performance prediction, failure theories have undergone numerous revisions. The current study uses the finite element method to predict the tensile response while also using Puck's failure criterion and the damage evolution law to composite laminates. Five non-hybrid sequences made of paperboard, ultra-high molecular weight polyethylene (UHMWPE), glass fibre, aramid fibre, and carbon fibre have been put through experimental investigation of tensile and three-point bending. The numerical analysis has been carried out using the Material Designer, ACP® and Structural Analysis modules of ANSYS® finite element software. The experimental results have been compared with the numerical results, to arrive at the set of empirical constants for the different materials.
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U2 - 10.1016/j.advengsoft.2022.103364
DO - 10.1016/j.advengsoft.2022.103364
M3 - Article
AN - SCOPUS:85142682275
SN - 0965-9978
VL - 175
JO - Advances in Engineering Software
JF - Advances in Engineering Software
M1 - 103364
ER -