19_beamelements

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Notes of beam element

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Beam Elements

Beam ElementsJake BlanchardSpring 2008Beam ElementsThese are Line Elements, with2 nodes6 DOF per node (3 translations and 3 rotations)Bending modes are included (along with torsion, tension, and compression)(there also are 2-D beam elements with 3 DOF/node 2 translations and 1 rotation)More than 1 stress at each point on the elementShape functionsAxial displacement is linear in xTransverse displacement is cubic in xCoarse mesh is often OKFor example, transverse displacement in problem pictured below is a cubic function of x, so 1 element can give exact solutionFBeam Elements in ANSYSBEAM 3 = 2-D elastic beamBEAM 4 = 3-D elastic beamBEAM 23 = 2-D plastic beamBEAM 24 = 3-D thin-walled beamBEAM 44 = 3-D elastic, tapered, unsymmetric beamBEAM 54 = 2-D elastic, tapered, unsymmetric beamBEAM 161 = Explicit 3-D beamBEAM 188 = Linear finite strain beamBEAM 189 = 3-D Quadratic finite strain beamReal ConstantsAreaIZZ, IYY, IXXTKZ, TKY (thickness)Theta (orientation about X)ShearZ, ShearY (accounts for shear deflection important for stubby beams)

Shear Deflection ConstantsshearZ=actual area/effective area resisting shearGeometryShearZ6/510/9212/5Shear Stresses in BeamsFor long, thin beams, we can generally ignore shear effects.To see this for a particular beam, consider a beam of length L which is pinned at both ends and loaded by a force P at the center.PL/2L/2Accounting for Shear Effects

Key parameter is height to length ratioDistributed LoadsWe can only apply loads to nodes in FE analysesHence, distributed loads must be converted to equivalent nodal loadsWith beams, this can be either force or moment loadsq=force/unit lengthMFFMDetermining Equivalent LoadsGoal is to ensure equivalent loads produce same strain energy

Equivalent Loads (continued)

MFFMPutting Two Elements TogetherMFFMMFFMMFFF2FMAn ExampleConsider a beam of length D divided into 4 elementsDistributed load is constantFor each element, L=D/4

qD/8qD/4qD/4qD/8qD/4qD2/192qD2/192In-Class ProblemsConsider a cantilever beamCross-Section is 1 cm wide and 10 cm tallE=100 GPaQ=1000 N/mD=3 m, model using surface load and 4 elementsD=3 m, directly apply nodal forces evenly distributed use 4 elementsD=3 m, directly apply equivalent forces (loads and moments) use 4 elementsD=20 cm (with and without ShearZ)

NotesFor adding distributed load, use Pressure/On BeamsTo view stresses, go to List Results/Element Results/Line elementsShearZ for rectangle is still 6/5Be sure to fix all DOF at fixed endNow Try a FrameF (out of plane)=1 N3 m2 mCross-sections6 cm5 cm