To verify the equilibrium of plate sections parallel to the supported edges based on shear stresses.
Anatoly V. Perelmuter, Vladimir I. Slivker. 'Design models of structures and the possibility of their analysis.' Moscow, DMK Press, 2007, pp. 238–240.
To determine the shear stresses τxz at the nodal points of the design model and verify that the area of the shear stress diagrams in the horizontal sections of the plate at y = 0; 2; 4; 6; 8; 10; 12; 14; 16 corresponds to the value of the horizontal reaction at point A.
A square plate is considered. Along the upper edge of the plate, a bar is placed that is absolutely rigid in bending and tension-compression. At point A (on the upper edge), the node is restrained against horizontal displacement. Along the lower edge, the plate is rigidly fixed. Two concentrated forces acting in opposite directions are applied to the plate.
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Variant 1
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Variant 2
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Plate thickness h = 1,0 m
Overall plate dimension a = 16 m
Modulus of elasticity Е = 3 * 105 kPa
Poisson's ratio ν = 0,25
Restraints in all degrees of freedom (DOF) of the FE are applied along the lower edge of the plate (X, Z, uY).
At point A, the node is restrained against horizontal displacement (X=0).
At the vertical centreline, the nodes are restrained against displacement along the Z-axis (Z=0).
Concentrated load P = 1000 kN
The problem is solved in a plane formulation (model type 2 – XOZ plane).
The model is generated with FE type 30 – arbitrary quadrilateral FE of 2D problem (wall-beam).
Variant 1:
Along the upper edge of the plate, the nodes are connected by kinematic restraints in the form of a perfectly rigid body (PRB).
Variant 2:
Along the upper edge of the plate, the nodes are connected by a fictitious bar with high bending and axial stiffness (EF = 3*1010 kN, EIy = 3*1010 kN*m2).
Finite element size: 2×2 m.
Nodes 81. Elements: 64.
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Variant 1
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Variant 2
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Variant 1
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Variant 2
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Variant 1
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Variant 2
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| The unknown | Point y, m | Analytical solution | LIRA-FEM | Error, % | ||
| Var. 1 | Var. 2 | Var. 1 | Var. 2 | |||
| Q, кН | 0 | 872,45 | 878,188 | 878,196 | 0,6534 | 0,6543 |
| 2 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
| 4 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
| 6 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
| 8 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
| 10 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
| 12 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
| 14 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
| 16 | 878,188 | 878,196 | 0,6534 | 0,6543 | ||
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Note: The area of shear stress diagrams in plate sections parallel to the supported edge and at a distance y from the simply supported edge is compared with the support reaction H. |
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