. . . . . "2"^^ . . "Analysis of Bonded Composite patch Using FEM" . "Ko\u0161ice" . . "Ko\u0161ice" . "1"^^ . "1"^^ . "2008-01-01+01:00"^^ . "RIV/60162694:G43__/08:00424136" . . "Nov\u00E9 trendy v rozvoji letectva" . "Analysis of Bonded Composite patch Using FEM"@en . . "Analysis of Bonded Composite patch Using FEM"@en . "978-80-553-0067-2" . "FEM; bonding; composite patch; shear stress"@en . "RIV/60162694:G43__/08:00424136!RIV11-MO0-G43_____" . "G43" . "Technick\u00E1 univerzita v Ko\u0161iciach" . . "S" . . "[7672F9C36371]" . "355776" . . "The aim of the work is to create a FEM model of bonded composite patch. The tension is put on analysing the adhesive shear stress that is crucial for the load capacity of the bonded joint. Included are influencing factors like adhesive fillet, thickness of the patch, the length of damage, symmetry of the joint and a chamfer of damaged plate. The goals of the work help to battle aircraft repairing in the field conditions."@en . "Hub, Juraj" . "The aim of the work is to create a FEM model of bonded composite patch. The tension is put on analysing the adhesive shear stress that is crucial for the load capacity of the bonded joint. Included are influencing factors like adhesive fillet, thickness of the patch, the length of damage, symmetry of the joint and a chamfer of damaged plate. The goals of the work help to battle aircraft repairing in the field conditions." . . . . . "Analysis of Bonded Composite patch Using FEM" .