To determine the stress–strain state of a circular plate.
S. Timoshenko, Résistance des matériaux, t. 2, Paris, Librairie Polytechnique Ch. Béranger, 1949.
To determine the vertical displacement Z (w) at the centre of the plate, as well as the bending moments at the clamped support.
A circular plate clamped along its contour subjected to a uniformly distributed load q.
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Radius of a plate r = 1,2 m.
Thickness h = 0,02 m;
Modulus of elasticity Å = 2,0 * 108 kPa.
Poisson's ratio ν = 0,3.
Restraints are applied along the outer contour of the plate for all degrees of freedom (DOF) of the slab finite element (Z, uX, uY).
Load uniformly distributed across the area: q = 10 kPa.
The problem is solved in a plane formulation (model type 3 – XOY-plane).
For model generation, FE 19 (quadrilateral FE of slab) and FE 12 (triangular Fe of slab) are used. These finite elements have three DOF per node: displacement along the global Z-axis and rotations about the global uX and uY axes.
The FE mesh consists of 12 elements along the radius and 48 elements along the circumference.
The local axes of the plate elements for result evaluation are oriented so that the Y1-axis is directed towards the centre of the circle (the Z1-axis is directed upwards).
Nodes: 577. Elements: 576.
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Design and deformed models (half of a plate is displayed) |
Contour plots of vertical displacements Z(w), mm |
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Mx = −qr2/8
My = −vqr2/8
Without additional side nodes:
| Point | The unknown | Analytic solution | LIRA-FEM | Error, % |
| Centre | Displacement w0, mm | -2,211 | -2,1938 | 0,7779 |
| Edge | Bending moment Mx, kN*m/m | 1,17 | 1,1549 | 1,2906 |
| Bending moment My, kN*m/m | 1,17 | 1,1519 | 1,547 |
With additional side nodes:
| Point | The unknown | Analytic solution | LIRA-FEM | Error, % |
| Centre | Displacement w0, mm | -2,211 | -2,2005 | 0,4749 |
| Edge | Bending moment Mx, kN*m/m | 1,17 | 1,1619 | 0,6923 |
| Bending moment My, kN*m/m | 1,17 | 1,1563 | 1,1709 |
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