Shear Locking

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    Manoj Chopade

    Roll No : 21ME Design (II Semester)

    Shear locking Phenomenon

    27thMay 2014

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    How Does Finite Element Analysis

    Work? The mathematical representation of

    the physical system in FEM is byusing nodes and elements.

    The process of creating nodes andelements is said as discretization or

    meshing. The number of degrees of freedom

    in each node depends on theelement type.

    As the FEM model has finite DOF as

    against infinite DOF in actualstructure, FEM solutions areapproximate and FEM model isstiffer

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    Shear locking Phenomenon

    Error called locking and how it is being overcome

    by the commercial FEA codes.

    In spite of providing approximate solutions to

    problems which cannot be solved analytically, there

    are some situations for which convergence is poor inFEM.

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    LOCKING :

    Locking means the effect of a reduced rate ofconvergence in dependence of a critical parameter.eg.slenderness of the plate in case of transverseshear locking.

    Because of locking , wrong displacements , falsestresses, spurious natural frequencies areencountered.

    Shear locking occurs on use of fully integratedlinear elements that are subjected to pure bending.The formulation of these elements promotes shearstrains that do not really exist

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    Shear locking:

    Timoshenko beam theory works for all l/d ratiowhereas Bernoullie beam theory works for only large

    values of l/d ratio.

    In thick beams , shear deformation becomes

    predominant and Bernoullis theory wont giveaccurate result.

    Shear locking occurs in elements which account for

    shear deformation ,when these elements are used in

    modeling bending predominant beams .

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    Shear locking occurs in elements which account for shear

    deformation ,when these elements are used in modeling bending

    predominant beams .

    A Cantilever beamsubjected to loading at the

    free end is analysed with

    the following properties :

    Youngs Modulus = 200GPa

    Poissons Ratio = 0.3

    Ansys Element SOLID 45

    and SOLID 185 is

    considered.

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    Meshing:

    L/d ratio = 25 L/d ratio = 5

    The beam is meshed such that there are 4 elements in height , 10 elements along

    the length and 1 element along the width.

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    The analytical solution for the tip deflection in case of a

    cantilever problem is calculated from

    P= Forceacting on the tip of the beam, L= Length of the beam (span) , E= Modulus of elasticity, I =Area moment of inertia

    The Answer obtained analytically for a cantilever beam of

    L/D ratio 25 is 0.312 cm The free end deflection obtained from SOLID45 is 0.308

    cm whereas from SOLID185 element the tip deflection is

    found to be 0.1514 cm .

    The difference between the results is due to shear locking

    and it is not an approximation error.

    ])(10.071.01[3

    3

    2

    23

    L

    D

    L

    D

    EI

    PLs

    http://en.wikipedia.org/wiki/Forcehttp://en.wikipedia.org/wiki/Span_(architecture)http://en.wikipedia.org/wiki/Modulus_of_elasticityhttp://en.wikipedia.org/wiki/Area_moment_of_inertiahttp://en.wikipedia.org/wiki/Area_moment_of_inertiahttp://en.wikipedia.org/wiki/Modulus_of_elasticityhttp://en.wikipedia.org/wiki/Span_(architecture)http://en.wikipedia.org/wiki/Forcehttp://en.wikipedia.org/wiki/Force
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    Shear Locking

    For a Beam in Pure Bending the shear strain is Zero

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    Tip deflection values in cm

    s.no L/D

    ratio

    ANALYTICAL

    SOLUTION

    SOLID 45 % Error SOLID185

    (reduced

    integration)

    1. 25 0.3128 0.308 50.8% 0.3328

    2. 20 0.16028 0.1578 39.6% 0.1705

    3. 15 0.0677 0.0667 26.68% 0.0720

    4. 10 0.02014 0.0196 26.28% 0.0214

    5. 5 0.002569 0.002523 6.8% 0.002757

    Compression Sheet

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    Interpretation of the results :

    It is clear from the table, as the beam thicknessincreases (as shear becomes predominant) the error

    is minimized.

    The error in the tip deflection values of bendingpredominant beams is due to Shear locking.

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    THANK YOU

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    References :

    Finite Element Analysis by C.S.Krishnamoorthy , IIT ,Madras.

    Strength of Materials- Elementary theory and problemsby Stephen Timoshenko

    Eric Quili Sun, Shear locking and hourglassing in MSC

    Nastran, Abaqus and Ansyswww.cmmacs.ernet.in/cmmacs/pdf/

    www.imechanica.org

    www.mscsoftware.com/events/vpd2006/na/presentations/

    .../27.pdfwww.eng-tips.org

    www.springerlink.com

    www.openpdf.com

    www.sciencedirect.com

    http://www.cmmacs.ernet.in/cmmacs/pdf/http://www.imechanica.org/http://www.mscsoftware.com/events/vpd2006/na/presentations/.../27.pdfhttp://www.mscsoftware.com/events/vpd2006/na/presentations/.../27.pdfhttp://www.eng-tips.org/http://www.springerlink.com/http://www.openpdf.com/http://www.sciencedirect.com/http://www.sciencedirect.com/http://www.openpdf.com/http://www.springerlink.com/http://www.eng-tips.org/http://www.eng-tips.org/http://www.eng-tips.org/http://www.mscsoftware.com/events/vpd2006/na/presentations/.../27.pdfhttp://www.mscsoftware.com/events/vpd2006/na/presentations/.../27.pdfhttp://www.imechanica.org/http://www.cmmacs.ernet.in/cmmacs/pdf/