A novel composite bolted joint element: application to a single-bolted joint

Procedia Structural Integrity - Tập 12 - Trang 281-295 - 2018
Valerio G. Belardi1, Pierluigi Fanelli2, Francesco Vivio1
1Department of Enterprise Engineering - University of Rome Tor Vergata, Via del Politecnico, 1, 00133, Rome, Italy
2Department of Economics, Engineering, Society and Business Organization, University of Tuscia, Largo dell’Università, 01100 Viterbo, Italy

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Belardi, 2018, Analysis of rectilinear orthotropic composite circular plates undergoing in-plane bending moment and torque through Ritz method, Composite Structures, 10.1016/j.compstruct.2018.05.062

Belardi, 2018, Bending analysis with Galerkin method of rectilinear orthotropic composite circular plates subject to transversal load, Composites Part B: Engineering, 140, 250, 10.1016/j.compositesb.2017.12.011

Belardi, 2018, Design, analysis and optimization of anisogrid composite lattice conical shells. Composites Part B: Engineering, 150, 184

Belardi, 2018, Elastic analysis of rectilinear orthotropic composite circular plates subject to transversal and in-plane load conditions using Ritz method, Composite Structures, 199, 63, 10.1016/j.compstruct.2018.05.062

Belardi, 2018, First-order shear deformation analysis of rectilinear orthotropic composite circular plates undergoing transversal loads, Under Review

Belardi, 2018, Structural analysis and optimization of anisogrid composite lattice cylindrical shells, Composites Part B: Engineering, 139, 203, 10.1016/j.compositesb.2017.11.058

Belardi, 2018, Structural analysis of transversally loaded quasi-isotropic rectilinear orthotropic composite circular plates with Galerkin method, Procedia Structural Integrity, 8, 368, 10.1016/j.prostr.2017.12.037

Chowdhury, 2016, Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures. Composites Part B: Engineering, 100, 68

Gray, 2010, A global bolted joint model for finite element analysis of load distributions in multi-bolt composite joints, Composites Part B: Engineering, 41, 317, 10.1016/j.compositesb.2010.03.001

Gray, 2011, A highly efficient user-defined finite element for load distribution analysis of large-scale bolted composite structures, Composites Science and Technology, 71, 1517

Jones, 1975

Kapidžić, 2014, Finite element modeling of mechanically fastened composite-aluminum joints in aircraft structures, Composite Structures, 109, 198, 10.1016/j.compstruct.2013.10.056

McCarthy, 2005, Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints: Part II effects of bolt-hole clearance. Composite Structures, 71, 159

McCarthy, 2005, Three-dimensional finite element analysis of single-bolt, single-lap composite bolted joints: part I - model development and validation. Composite Structures, 71, 140

Reddy, 2006

Vivio, 2009, A new theoretical approach for structural modelling of riveted and spot welded multi-spot structures, International Journal of Solids and Structures, 46, 4006, 10.1016/j.ijsolstr.2009.07.021

Zhou, 2015, A three dimensional implicit finite element damage model and its application to single-lap multi-bolt composite joints with variable clearance, Composite Structures, 131, 1060, 10.1016/j.compstruct.2015.06.073