Fourier solution to higher order theory based laminated shell boundary-value problem
A complete Fourier solution to the boundary-value problem of static response under transverse load of a general cross-ply thick doubly curved panel of rectangular planform is presented.
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Veröffentlicht in: | AIAA journal 1995-09, Vol.33 (9), p.1681-1688 |
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container_issue | 9 |
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container_title | AIAA journal |
container_volume | 33 |
creator | Chaudhuri, Reaz A Kabir, Humayun R. H |
description | A complete Fourier solution to the boundary-value problem of static response under transverse load of a general cross-ply thick doubly curved panel of rectangular planform is presented. |
doi_str_mv | 10.2514/3.12498 |
format | Article |
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ispartof | AIAA journal, 1995-09, Vol.33 (9), p.1681-1688 |
issn | 0001-1452 1533-385X |
language | eng |
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source | Alma/SFX Local Collection |
subjects | Civil engineering Composite materials Exact sciences and technology Fundamental areas of phenomenology (including applications) Physics Solid mechanics Static elasticity Static elasticity (thermoelasticity...) Structural and continuum mechanics |
title | Fourier solution to higher order theory based laminated shell boundary-value problem |
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