2015
DOI: 10.13111/2066-8201.2015.7.1.8
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Buckling of Flat Thin Plates under Combined Loading

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Cited by 3 publications
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“…The general equation of the sheet considering different boundary conditions including simply supported (hinged), clamped (fixed) edges, and single or combined loading of bending, compression, and shear can be written as. 17,19 Where N x , N y , and N xy are the critical distributed flow forces (N/mm); w is the displacement in the normal direction on the sheet; t is the thickness of the sheet (mm), and D is the bending stiffness of the sheet. The normal and shearing stresses can be defined as: Transverse stiffeners are also important to be considered to preserve the straight boundaries for computing the shear buckling of the plate.…”
Section: Buckling Deformationmentioning
confidence: 99%
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“…The general equation of the sheet considering different boundary conditions including simply supported (hinged), clamped (fixed) edges, and single or combined loading of bending, compression, and shear can be written as. 17,19 Where N x , N y , and N xy are the critical distributed flow forces (N/mm); w is the displacement in the normal direction on the sheet; t is the thickness of the sheet (mm), and D is the bending stiffness of the sheet. The normal and shearing stresses can be defined as: Transverse stiffeners are also important to be considered to preserve the straight boundaries for computing the shear buckling of the plate.…”
Section: Buckling Deformationmentioning
confidence: 99%
“…The following formulas for the corresponding buckling stresses are obtained. 19 Where σ c c , 0 is the critical single compression stress; τ c r , 0 is the critical single shear stress; σ c f , 0 is the critical single bending stress; η is the plasticity factor; E is the Young's modulus (N/mm 2 ), while K is the buckling factor, which equals to K = k false( π 2 .1em 12 false( 1 v e 2 false) false) , where k is given depending on ( a / b ) ratio. If the sheet is loaded with a transverse compression stress (as per y ), then b should be replaced by (a) in Equation (3).…”
Section: Buckling Deformationmentioning
confidence: 99%
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