composite laminates;
crack-tip force method;
delamination;
energy release rate;
laminated plates;
virtual crack closure technique;
D O I:
10.1016/S0263-8223(01)00170-2
中图分类号:
O3 [力学];
学科分类号:
08 ;
0801 ;
摘要:
A new method called the crack-tip force method (CTFM) is derived for computing the energy release rate in delaminated beams and plates. In this method the delaminated plate is divided into two laminates on either side of the plane of delamination. The interaction forces, called crack-tip forces, between the sub-laminates at the crack-tip are computed. The energy release rate is expressed as a quadratic function of the crack-tip forces and the plate compliance coefficients. The CTFM is compared to the virtual crack closure technique (VCCT) as well as to a previously derived method called the strain energy density method using double cantilevered beam specimens as examples. The CTFM is found to be very efficient as the crack-tip forces are part of the solution of finite element analysis of delaminated plates, and they can be readily used to compute the point-wise energy release rate along the delamination front. (C) 2002 Elsevier Science Ltd. All rights reserved.
机构:Department of Aerospace Engineering, Mechanics, and Engineering Sciences, Center for Studies of Advanced Structural Composites, University of Florida, Gainesville, FL
SANKAR, BV
;
SONIK, V
论文数: 0引用数: 0
h-index: 0
机构:Department of Aerospace Engineering, Mechanics, and Engineering Sciences, Center for Studies of Advanced Structural Composites, University of Florida, Gainesville, FL
机构:Department of Aerospace Engineering, Mechanics, and Engineering Sciences, Center for Studies of Advanced Structural Composites, University of Florida, Gainesville, FL
SANKAR, BV
;
SONIK, V
论文数: 0引用数: 0
h-index: 0
机构:Department of Aerospace Engineering, Mechanics, and Engineering Sciences, Center for Studies of Advanced Structural Composites, University of Florida, Gainesville, FL