Computation of interlaminar stresses from finite element solutions to plate theories

Interlaminar stresses are estimated from plate theories by equilibrium. The elasticity equations of equilibrium are integrated with respect to the thickness coordinate z using the linear distribution in z of the in-plane stresses. This procedure, for example, requires fourth order derivatives of the...

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Main Author: Foster, John L.
Other Authors: Aerospace Engineering
Format: Others
Language:en
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/35814
http://scholar.lib.vt.edu/theses/available/etd-11242009-020113/
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-358142021-05-08T05:26:58Z Computation of interlaminar stresses from finite element solutions to plate theories Foster, John L. Aerospace Engineering Johnson, Eric R. Griffin, Odis Hayden Jr. Kapania, Rakesh K. LD5655.V855 1991.F687 Laminated materials -- Research Interlaminar stresses are estimated from plate theories by equilibrium. The elasticity equations of equilibrium are integrated with respect to the thickness coordinate z using the linear distribution in z of the in-plane stresses. This procedure, for example, requires fourth order derivatives of the out-of-plane displacement w with respect to the in-plane coordinates x and y to compute the interlaminar normal stress. Since compatible elements for the plate bending problem at most require the displacement and its first derivatives to be continuous across element boundaries, low degree interpolation polynomials are used. Thus, fourth order derivatives of the finite element polynomials are either meaningless, or at least inaccurate. In order to compute high order derivatives, an approximate polynomial solution of high degree to the governing partial differential equation for w(x,y) is determined using the finite element solution as a first approximation. A rectangular subdomain that may consist of several elements is selected from the finite element model. The displacement w(,y) over the subdomain is expanded in a Chebyshev series. Then collocation is used to determine the unknown Chebyshev coefficients such that the Chebyshev series matches displacement w and its normal derivative from the finite element solution at discrete points on the boundary of the subdomain, and the partial differential equation is enforced at discrete points within the subdomain. Interlaminar shear and normal stresses are computed from the third and fourth derivatives, respectively, of the Chebyshev series at the collocation points. Master of Science 2014-03-14T20:48:20Z 2014-03-14T20:48:20Z 1991-04-01 2009-11-24 2011-10-19 2009-11-24 Thesis Text etd-11242009-020113 http://hdl.handle.net/10919/35814 http://scholar.lib.vt.edu/theses/available/etd-11242009-020113/ en OCLC# 23991296 LD5655.V855_1991.F687.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ vii, 82 leaves BTD application/pdf application/pdf Virginia Tech
collection NDLTD
language en
format Others
sources NDLTD
topic LD5655.V855 1991.F687
Laminated materials -- Research
spellingShingle LD5655.V855 1991.F687
Laminated materials -- Research
Foster, John L.
Computation of interlaminar stresses from finite element solutions to plate theories
description Interlaminar stresses are estimated from plate theories by equilibrium. The elasticity equations of equilibrium are integrated with respect to the thickness coordinate z using the linear distribution in z of the in-plane stresses. This procedure, for example, requires fourth order derivatives of the out-of-plane displacement w with respect to the in-plane coordinates x and y to compute the interlaminar normal stress. Since compatible elements for the plate bending problem at most require the displacement and its first derivatives to be continuous across element boundaries, low degree interpolation polynomials are used. Thus, fourth order derivatives of the finite element polynomials are either meaningless, or at least inaccurate. In order to compute high order derivatives, an approximate polynomial solution of high degree to the governing partial differential equation for w(x,y) is determined using the finite element solution as a first approximation. A rectangular subdomain that may consist of several elements is selected from the finite element model. The displacement w(,y) over the subdomain is expanded in a Chebyshev series. Then collocation is used to determine the unknown Chebyshev coefficients such that the Chebyshev series matches displacement w and its normal derivative from the finite element solution at discrete points on the boundary of the subdomain, and the partial differential equation is enforced at discrete points within the subdomain. Interlaminar shear and normal stresses are computed from the third and fourth derivatives, respectively, of the Chebyshev series at the collocation points. === Master of Science
author2 Aerospace Engineering
author_facet Aerospace Engineering
Foster, John L.
author Foster, John L.
author_sort Foster, John L.
title Computation of interlaminar stresses from finite element solutions to plate theories
title_short Computation of interlaminar stresses from finite element solutions to plate theories
title_full Computation of interlaminar stresses from finite element solutions to plate theories
title_fullStr Computation of interlaminar stresses from finite element solutions to plate theories
title_full_unstemmed Computation of interlaminar stresses from finite element solutions to plate theories
title_sort computation of interlaminar stresses from finite element solutions to plate theories
publisher Virginia Tech
publishDate 2014
url http://hdl.handle.net/10919/35814
http://scholar.lib.vt.edu/theses/available/etd-11242009-020113/
work_keys_str_mv AT fosterjohnl computationofinterlaminarstressesfromfiniteelementsolutionstoplatetheories
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