TY - JOUR
T1 - Edge debonding in patched cylindrical panels
AU - Bottega, W. J.
AU - Loia, M. A.
N1 - Funding Information:
Acknawledgement-The authors wish to thank D. W. Oplinger of the Federal Aviation Administration for his support and encouragement. This work was supported by the FAA through the Rutgers University Center for Computational Modeling of Aircraft Structures (CMAS).
PY - 1996/10
Y1 - 1996/10
N2 - Circumferential edge debonding is considered for structural configurations corresponding to patched cylindrical panels, under a variety of loading conditions. These include applied circumferential tension, radial three-point loading, and applied pressure. The effect of support conditions on the evolution of the composite structure is also examined as are the effects of relative stiffness and arc length of the patch with respect to those of the base panel. The problems are approached from a unified point of view, as a moving interior boundaries problem in the calculus of variations, resulting in a self-consistent model of the intact and debonded segments of the composite structure, the individual primitive structures, and the corresponding conditions which define the intermediate boundaries of the bonded region and a region of sliding contact. Numerical simulations based on analytical solutions reveal characteristic behavior of the evolving structure under load.
AB - Circumferential edge debonding is considered for structural configurations corresponding to patched cylindrical panels, under a variety of loading conditions. These include applied circumferential tension, radial three-point loading, and applied pressure. The effect of support conditions on the evolution of the composite structure is also examined as are the effects of relative stiffness and arc length of the patch with respect to those of the base panel. The problems are approached from a unified point of view, as a moving interior boundaries problem in the calculus of variations, resulting in a self-consistent model of the intact and debonded segments of the composite structure, the individual primitive structures, and the corresponding conditions which define the intermediate boundaries of the bonded region and a region of sliding contact. Numerical simulations based on analytical solutions reveal characteristic behavior of the evolving structure under load.
UR - http://www.scopus.com/inward/record.url?scp=0030269085&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0030269085&partnerID=8YFLogxK
U2 - 10.1016/0020-7683(95)00205-7
DO - 10.1016/0020-7683(95)00205-7
M3 - Article
AN - SCOPUS:0030269085
SN - 0020-7683
VL - 33
SP - 3755
EP - 3777
JO - International Journal of Solids and Structures
JF - International Journal of Solids and Structures
IS - 25
ER -