Theories of elastic plates

Gebonden Engels 1975 9789028601048
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Samenvatting

The present monograph deals with refined theories of elastic plates in which both bending and transverse shear effects are taken into account and with some of their applications. Generally these more exact theories result in inte­ gration problems of the sixth order; consequently, three mutually independent boundary conditions at each edge of the plate are required. This is in perfect agreement with the conclusions of the theory of elasticity. The expressions for shearing forces following from refined theories are then valid for the whole investigated region including its boundary where the corresponding boundary conditions for these shearing forces can be prescribed. Quite different seems to be the situation in the classical Kirchhoff-Love's theory in which the influence of transverse shearing strains is neglected. Owing to this simplification the governing differential equation developed by the classical theory is of the fourth order only; consequently, the number of boundary conditions appurtenant to the applied mode of support appears now to be in disagreement with the order of the valid governing equation. Then, limiting the validity of the expressions for shearing forces to the open region of the middle plane and introducing the notion of the so called fictitious Kirchhoff's shearing forces for the boundary of the plate, three actual boundary conditions at each edge of the plate have to be replaced by two approximate conditions transformed in the Kirchhoff's sense.

Specificaties

ISBN13:9789028601048
Taal:Engels
Bindwijze:gebonden
Uitgever:Springer Netherlands

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Inhoudsopgave

1 Basic relations in theories of elastic plates.- I Isotropic rectangular plates.- 2 Differential equations of the component theory.- 2.1 Summary of basic equations.- 2.2 Transformation of basic equations for resultant quantities.- 2.3 Some special cases.- 3 The Reissner plate theory.- 3.1 Summary of governing equations.- 3.2 Neglecting transverse contraction in the Reissner theory.- 4 Refined theory of Hencky.- 4.1 Summary of governing equations.- 4.2 Modification of the Hencky theory based on more accurate displacement functions.- 5 Refined theory of Kromm.- 5.1 Bending state.- 5.1.1 Cases p = const., p = 0. Comparison with the component theory.- 5.1.2 Case of a general harmonic load.- 5.1.3 Particular solution for a general non-harmonic load.- 5.1.4 Comparison with the second approximation of the component theory.- 5.2 Antisymmetric stress state of the plate without deflections.- 5.2.1 Comparison with the third approximation of the component theory.- 5.3 Satisfaction of Kromm’s equations in their integral form.- 6 Generalized theory.- 6.1 Summary of governing equations.- 6.2 Process of solution.- 6.3 Comparison with other refined theories.- 7 Boundary conditions.- 7.1 Boundary conditions in refined theories.- 7.1.1 Free edge.- 7.1.2 Simply supported edge.- 7.1.3 Elastically supported edge.- 7.1.4 Built-in edge.- 7.1.5 Elastically built-in edge.- 7.1.6 Continuous plate.- 7.1.7 Elastically supported continuous plate.- 7.1.8 Continuous plate on elastically rotating supports.- 7.1.9 Curvilinear edge.- 7.2 Boundary conditions leading to integration problems of the fourth order.- 7.2.1 Basic relations for resultant quantities of the second approximation of the component theory.- 7.2.2 Basic relations for particular solutions defined by the generalized theory.- 7.2.3 Free edge.- 7.2.4 Simply supported edge.- 7.2.5 Built-in edge.- 8 Bending of long rectangular plates to a cylindrical surface.- 8.1 General solution following from the component theory.- 8.1.1 Cantilever.- 8.1.2 Strip with simply supported edges.- 8.1.3 Strip with built-in edges.- 8.1.4 Strip with one edge simply supported and other edge built-in.- 8.1.5 Continuous plate strip.- 8.2 General solution following from the generalized theory.- 8.2.1 Cantilever.- 8.2.2 Strip with simply supported edges.- 8.2.3 Strip with built-in edges.- 8.2.4 Strip with one edge simply supported and other edge built-in.- 8.2.5 Continuous plate strip.- 9 Solution of the boundary value problem for a rectangular plate.- 10 Plate with two opposite edges simply supported.- 10.1 Bending by moments distributed along one simply supported edge.- 10.1.1 Deformation symmetrical with respect to both coordinate axes.- 10.1.2 Deformation symmetrical with respect to the x-axis and antisym- metrical to the y-axis.- 10.1.3 Deformation symmetrical with respect to the y-axis and antisymmetri- cal to the x-axis.- 10.1.4 Deformation antisymmetrical with respect to both coordinate axes.- 10.2 Bending by moments distributed along one free edge.- 10.2.1 Deformation symmetrical with respect to both coordinate axes.- 10.2.2 Deformation symmetrical with respect to the y-axis and antisymmetrical to the x-axis.- 10.2.3 Deformation symmetrical with respect to the x-axis and antisymmetrical to the y-axis.- 10.2.4 Deformation antisymmetrical with respect to both coordinate axes.- 10.3 Bending by shearing forces distributed along one free edge.- 10.3.1 Deformation symmetrical with respect to both coordinate axes.- 10.3.2 Deformation symmetrical with respect to the y-axis and antisymmetrical to the x-axis.- 10.3.3 Deformation symmetrical with respect to the x-axis and antisymmetrical to the y-axis.- 10.3.4 Deformation antisymmetrical with respect to both coordinate axes.- 11 Free rectangular plate.- 11.1 Bending by moments distributed along the edges.- 11.1.1 Deformation symmetrical with respect to both coordinate axes.- 11.1.1.1 Influence of the boundary moment distribution and of the thickness on deflections of a square plate. Numerical comparison.- 11.1.2 Deformation symmetrical with respect to the x-axis and antisymmetrical to the y-axis.- 11.1.3 Deformation symmetrical with respect to the y-axis and antisymmetrical to the x-axis.- 11.2 Bending by twisting moments distributed along the edges.- 11.2.1 Deformation antisymmetrical with respect to both coordinate axes.- 11.2.1.1 Influence of the distribution of boundary twisting moments and of the plate thickness.- 11.2.2 Deformation symmetrical with respect to both coordinate axes.- 11.2.2.1 Influence of plate thickness on deflections.- 12 Simply supported plate subjected to boundary bending moments.- 12.1 Deformation symmetrical with respect to both coordinate axes.- 12.1.1 Influence of plate thickness on the maximum deflection. Comparison with the classical theory.- 12.2 Deformation symmetrical with respect to the x-axis and antisymmetrical to the y-axis.- 12.3 Deformation symmetrical with respect to the y-axis and antisymmetrical to the x-axis.- 12.4 Deformation antisymmetrical with respect to both coordinate axes.- 13 Completely simply supported plate under distributed loading.- 13.1 Solution according to the component theory.- 13.1.1 Square plate. Influence of the plate thickness and of the number of terms considered.- 13.2 Solution according to the generalized theory.- 13.2.1 Square plate.- 14 Completely built-in plate under distributed loading.- 14.1 Solution according to the component theory.- 14.1.1 Square plate. Influence of the plate thickness. Comparison with the classical theory.- 14.2 Solution according to the generalized theory.- 15 Plate with two opposite edges simply supported and the other two edges free under a continuous load.- 15.1 Solution according to the component theory.- 15.2 Solution according to the generalized theory.- 16 Plate with two opposite edges simply supported and the other two edges built-in under a continuous load.- 16.1 Solution according to the component theory.- 16.2 Solution according to the generalized theory.- II Orthotropic rectangular plates.- 17 Differential equations of the component theory. Case H= (KxKy)½.- 17.1 Summary of governing equations.- 17.2 Transformation of governing equations for resultant quantities.- 17.3 Transformation of coordinates.- 18 Generalized theory.- 18.1 Summary of governing equations.- 18.2 Governing equations for the case H = (KxKy)½.- 19 Refined theory developed by K. Girkmann and R. Beer.- 19.1 Summary of governing equations.- 19.2 Neglect of transverse contraction. Comparison with the generalized theory.- 19.3 Governing equations for the ease H = (KxKy)½ Comparison with the component theory.- 20 General solution of the boundary value problem according to the component theory.- 21 Orthotropic rectangular plate under a continuous load.- 21.1 Cantilever.- 21.2 Plate with one edge built-in, the opposite edge free, and the other edges simply supported.- 21.3 Plate with three edges built-in and one edge free.- 21.4 Plate with one edge built-in, the opposite edge free, and the other edges elastically built-in.- 21.5 Plate with three edges simply supported and one edge free.- 21.6 Plate with one edge simply supported, the opposite edge free, and the other edges built-in.- III Isotropic circular plates.- 22 Differential equations of the component theory in cylindrical coordinates.- 22.1 Summary of governing equations.- 22.2 Transformation of governing equations for resultant quantities.- 22.3 Alternate method of derivation of governing equations.- 23 Generalized theory of circular plates.- 23.1 Procedure of solution.- 23.2 Case ?rp = 0.- 24 Rotationally symmetrical bending.- 24.1 General solution of governing equations.- 24.2 Particular solutions for some continuously distributed loads.- 25 Circular plates under rotationally symmetrical loads.- 25.1 Bending by moments uniformly distributed along the edge.- 25.2 Uniformly loaded circular plate.- 25.2.1 Simply supported edge.- 25.2.2 Absolutely built-in edge.- 25.2.3 Elastically built-in edge.- 25.3 Circular plate under a partial uniform load.- 25.3.1 Simply supported edge.- 25.3.2 Built-in edge.- 26 Annular plates under rotationally symmetrical loads.- 26.1 Simply supported outer edge.- 26.2 Both edges simply supported.- 26.3 Both edges built-in.- 27 General solution of governing equations of the component theory for loads distributed according to the law p?(?) sin n ?.- 27.1 Formulae for differentiation of modified Bessel functions.- 27.2 Case n = 1.- 27.3 Case n = 2.- 28 Antisymmetrical bending of a circular plate under the load ?? sin ?.- 28.1 Simply supported edge.- 28.2 Built-in edge.- 28.3 Elastically built-in edge.- IV Circular plates on elastic foundation under rotationally symmetrical loads.- 29 Governing equations of the component theory.- 29.1 Introduction of a new dimensionless variable.- 29.2 General solution of the governing equation.- 29.2.1 Case x 1.- 29.3 Two-parameter elastic foundation.- 30 Auxiliary formulae for Bessel functions.- 30.1 Functions of complex arguments.- 30.2 Functions of pure imaginary arguments.- 31 Functions expressing the general solution of the homogeneous problem.- 31.1 Case x < 1.- 31.2 Case x = 1.- 31.3 Case x > 1.- 32 Fundamental solution.- 32.1 Case x < 1.- 32.1.1 Infinite plate under a concentrated load.- 32.1.2 Load uniformly distributed along a circle.- 32.1.3 Load uniformly distributed over an annular surface.- 32.1.4 Load uniformly distributed over a circular surface.- 32.2 Case x = 1.- 32.2.1 Infinite plate under a concentrated load.- 32.2.2 Load uniformly distributed along a circle.- 32.2.3 Load uniformly distributed over an annular surface.- 32.2.4 Load uniformly distributed over a circular surface.- 32.3 Case x > 1.- 32.3.1 Infinite plate under a concentrated load.- 32.3.2 Load uniformly distributed along a circle.- 32.3.3 Load uniformly distributed over an annular surface.- 32.3.4 Load uniformly distributed over a circular surface.- 32.4 Effect of the parameter x on deflection of an infinite plate under a concentrated load.- 33 Compensating solution.- 33.1 Circular plate.- 33.1.1 Free edge.- 33.1.1.1 Case x < 1.- 33.1.1.2 Case x = 1.- 33.1.1.3 Case x > l.- 33.1.2 Simply supported edge.- 33.1.2.1 Case x < 1.- 33.1.2.2 Case x = 1.- 33.1.2.3 Case x > 1.- 33.1.3 Built-in edge.- 33.1.3.1 Case x < 1.- 33.1.3.2 Case x = 1.- 33.1.3.3 Case x > 1.- 33.2 Infinite plate with a circular hole.- 33.3 Annular plate.- 34 Numerical example.- 34.1 Case x = 0.- 34.2 Case x = 0.17365.- 34.3 Case x= 1.0.- 34.4 Case x = 2.125.- Author index.

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