(1.9.1)--6.10 Chapter Sumary and Review材料力学材料力学.ppt
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1、 Mechanics of MaterialsChapter Sumary and ReviewChapter 6 Stresses in Beams(Advanced Topics)Welcome to Mechanics of Materials.This Chapter presented a number of specialized topics related to the bending of beams,including the analysis of composite beams,beams with inclined loads,unsymmetric beams,sh
2、ear stresses in thin-walled beams,and shear centers.This section gives some of the major concepts and findings presented in this chapter.1.Composite beams Moment-curvaturerelationship:Flexureformulasforcompositebeamsoftwomaterials:In the introduction to composite beams,specialized moment-curvature r
3、elationship and flexure formulas for composite beams of two materials were developed.Both materials must follow Hookes law,and the two parts of the beam must be adequately bonded so that they act as a single unit.The formulas here do not apply to reinforced concrete beams,which are not designed on t
4、he basis of linearly elastic behavior.Themodularratio:Themomentofinertiaofthetransformedsection:Thesimplifiedflexureformula:2.Transformed-section method A1A2The transformed-section method offers a convenient way of transforming the cross section of a composite beam into an equivalent cross section o
5、f an imaginary beam that is composed of only one material.With the introduction of the modular ratio n and the moment of inertia of the transformed section,a simplified flexure formula is given.3.Inclined load yzF Fz zF Fy yF F Analytical ProcedureSuperposition:Twoplanebendingareanalysedseparatelyan
6、dthecorrespondingresultsaresuperposed.Decomposition:DecomposetheloadalongthetwoCentroidalprincipalaxesofthecrosssectiontoobtaintwoorthogonalplanebending.If inclined loads act through the centroid of the cross section of beams with two axes of symmetry in the cross section,there will be no twisting o
7、f the beam about the longitudinal axis.For these beams,compute the bending stresses by resolving the inclined load into two componentsone acting in each plane of symmetry.The bending stresses were obtained from the flexure formula for each load component acting separately,and the final stresses obta
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- 1.9.1-6.10 Chapter Sumary and Review材料力学材料力学 1.9 6.10 Review 材料力学
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