improved transverse shear deformation theory for laminated anisotropic plates
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improved transverse shear deformation theory for laminated anisotropic plates

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Published by National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va .
Written in English

Subjects:

  • Deformations (Mechanics),
  • Laminated materials,
  • Strains and stresses

Book details:

Edition Notes

StatementM.V.M. Murthy
SeriesNASA technical paper -- 1903
ContributionsLangley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
The Physical Object
Pagination36 p. :
Number of Pages36
ID Numbers
Open LibraryOL14932993M

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An improved transverse shear deformation theory for laminated anisotropic plates under bending is presented. The theory eliminates the need for an arbitrarily chosen shear correction factor. For a general laminate with coupled bending and stretching, the constitutive equations connecting resultants with average displacements and rotations are by: 4.   Transverse shear in laminated plate theories. Transverse shear stiffness of laminated anisotropic shells. Computer Methods in Applied Mechanics and Engineering, Vol. 13, No. 2. Recommended. An improved shear deformation theory for laminated shells addressing transverse stress by: An improved transverse shear deformation theory for laminated anisotropic plates under bending is presented. The theory eliminates the need for an arbitrarily chosen shear correction factor. For a general laminate with coupled bending and stretching, the constitutive equations connecting resultants with average displacements and rotations are Author: M. V. V. Murthy. Plate Theory Elastic Plate Anisotropic Plate Transverse Shear Deformation Refined Theory These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm by:

In the present study, a new higher order shear deformable laminated composite plate theory is proposed. It is constructed from 3-D elasticity bending solutions by using an inverse method. Present theory exactly satisfies stress boundary conditions on the top and the bottom of the by: Soldatos, K. P. [] “ A transverse shear deformation theory for homogeneous monoclinic plates,” Acta Mechanica 94(3/4), – Crossref, ISI, Google Scholar; Soldatos, K. P. and Elishakoff, I. [] “ A transverse shear and normal deformable orthotropic beam theory,” Journal of Sound and Vibration (3), –Cited by:   A bending theory which includes transverse shear deformations is presented for laminated plates. Closed form solutions are obtained for bending deflections, flexural vibration frequencies, and buckling loads of simply-supported rectangular plates of special by: A new higher order shear deformation theory for sandwich and composite laminated plates Composites Part B: Engineering, Vol. 43, No. 3 A new trigonometric layerwise shear deformation theory for the finite element analysis of laminated composite and sandwich platesCited by:

Get this from a library! An improved transverse shear deformation theory for laminated anisotropic plates. [M V V Murthy; Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.]. An Improved Shear-Deformation Theory for Moderately Thick Multilayered Anisotropic Shells and Plates M. Di Sciuva. M. Di Sciuva. The general linear equations governing the motion of moderately thick multilayered anisotropic shells are derived by making use of the principle of virtual work in conjunction with an a priori assumed displacement Cited by:   A review of displacement and stress based refined theories for isotropic and anisotropic laminated plates is presented. A Review of Refined Shear Deformation Theories of Isotropic and Anisotropic Laminated Plates. , “An Improved Transverse Shear Deformation Theory for Laminated Anisotropic plates,” NASA Tech. Paper , pp. 1 Cited by: The present theory for symmetric laminated composites is obtained by superimposing a cubic varying displacement field on a zigzag linearly varying displacement satisfies transverse shear stress continuity conditions at the interface between layers as well as shear free surface condi- by: