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 EXAMPLE 1. Lateral Buckling of a Circular Annular Plate under Uniform Shearing Forces Applied at its Edges 1.1 Description of the Test A circular annular plate is subjected to a uniform shearing f orces applied at it s edges. Plate geometric and material properties are shown in Fig. 1.1a. Note: Effect of uniform shearing forces applied on plate edges is reproduced in finite element analysis by applying a drilling moment  Z  M  at the master node located at centroid of the  plate (origin of the coordinate axes). All six DOF’s of the nodes located on internal edge of the plate are connected by rigid body link to master node. 1.2 Comparison of  the Results According to Dean [1], for the annular plate with material and geometric properties, illustrated in Fig. 1.1a, the analytical solution of critical moment cr  M  is defined by the following value: cr  M  = 230,500 kN×m Finite element solution of cr  M  is computed for a regular mesh 10×60 (see Fig. 1.1b), using 4- node quadrilateral shell FE with dr illing DOF, and is reported in Table 1. The obtained results are compared with target solution reported in Dean [1]. Table 1 Comparison of the Critical Moment cr  M   for a Circular Annular Plate under Uniform Shearing Forces FE Type Dean [1] MIDAS/Civil SAP2000 Thin Shell 240,015.5 240,015.5 Thick Shell 230,500 230,500.0 230,500.0

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  • EXAMPLE 1. Lateral Buckling of a Circular Annular Plate under Uniform Shearing Forces Applied at its Edges

    1.1 Description of the Test A circular annular plate is subjected to a uniform shearing forces applied at its edges. Plate

    geometric and material properties are shown in Fig. 1.1a.

    Note: Effect of uniform shearing forces applied on plate edges is reproduced in finite element

    analysis by applying a drilling moment ZM at the master node located at centroid of the

    plate (origin of the coordinate axes). All six DOFs of the nodes located on internal edge

    of the plate are connected by rigid body link to master node.

    1.2 ComparisonoftheResults

    According to Dean [1], for the annular plate with material and geometric properties, illustrated in

    Fig. 1.1a, the analytical solution of critical moment crM is defined by the following value:

    crM = 230,500 kNm

    Finite element solution of crM is computed for a regular mesh 1060 (see Fig. 1.1b), using 4-

    node quadrilateral shell FE with drilling DOF, and is reported in Table 1. The obtained results

    are compared with target solution reported in Dean [1].

    Table 1 Comparison of the Critical Moment crM for a Circular Annular Plate under Uniform Shearing Forces

    FE Type Dean [1] MIDAS/Civil SAP2000

    Thin Shell 240,015.5 240,015.5

    Thick Shell 230,500

    230,500.0 230,500.0

  • Geometric properties: Material properties: Ro = 5.0 m E = 2.1108 kN/m2 Ri = 2.5 m = 0.3 t = 0.1 m

    a) General View

    Figure 1.1 Circular Annular Plate Subjected to Uniform Sheering Forces (Continued)

  • b) Finite Element Model

    Figure 1.1 Circular Annular Plate Subjected to Uniform Sheering Forces

  • Mode 1

    Mode 3 Figure 1.2 Different Modes of Buckled Shapes

  • 1.3 References

    1. Dean, W. R., (1924). The Elastic Stability of an Annular Plate, Proc. Royal Society of London. Series A, Papers of a Mathematical and Physical Character, Vol. 106, No. 737, 268-284