Stability study of composite panels

The buckling behaviour of composite plate, three-strip composite panel in the shape of plain channel and five-strip comf)osite panel in the shape of lipped channel made of symmetric and antisymmetric angle-ply laminates is studied using the Finite Strip Method. The laminated composite panels under s...

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Main Author: Toh, Hoong Thiam.
Other Authors: Khong, Poh Wah
Format: Theses and Dissertations
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/19850
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-198502023-03-11T17:29:27Z Stability study of composite panels Toh, Hoong Thiam. Khong, Poh Wah School of Mechanical and Production Engineering DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics The buckling behaviour of composite plate, three-strip composite panel in the shape of plain channel and five-strip comf)osite panel in the shape of lipped channel made of symmetric and antisymmetric angle-ply laminates is studied using the Finite Strip Method. The laminated composite panels under study are subjected to in-plane uniform compression load. Three different boundary conditions of the loaded edges are considered. In the first case, both the loaded edges are simply supported. In the second case both the loaded edges are clamped. In the third case, one of the edges is simply supported while the other is clamped. In all cases the unloaded edges of the composite plate are simply supported whereas those of the three-strip composite panel and five-strip composite panel are fi-ee. Displacement function comprises a quintic polynomial in the transverse direction and a 10-term Chebyshev polynomial in the longitudinal direction is chosen to model the out-of-plane deflection. Comparison is made against the displacement fiinction which use trigonometric function in the longitudinal direction. A FORTRAN program has been developed to generate the desired results. The validity of the results obtained are verified by comparing with published results. Geometric parametric studies such as the effect of flange width to web width ratio on the buckling behaviour of composite panels of plain channel and lipped channel shapes is illustrated. In addition, the effect of lip to flange ratio on the buckling behaviour of five-strip composite panel in the shape of lipped channel is also investigated. The advantage of using Chebyshev polynomial over trigonometric function is also discussed. Master of Science (Mechanical Engineering) 2009-12-14T06:50:55Z 2009-12-14T06:50:55Z 1995 1995 Thesis http://hdl.handle.net/10356/19850 en NANYANG TECHNOLOGICAL UNIVERSITY 223 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics
spellingShingle DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics
Toh, Hoong Thiam.
Stability study of composite panels
description The buckling behaviour of composite plate, three-strip composite panel in the shape of plain channel and five-strip comf)osite panel in the shape of lipped channel made of symmetric and antisymmetric angle-ply laminates is studied using the Finite Strip Method. The laminated composite panels under study are subjected to in-plane uniform compression load. Three different boundary conditions of the loaded edges are considered. In the first case, both the loaded edges are simply supported. In the second case both the loaded edges are clamped. In the third case, one of the edges is simply supported while the other is clamped. In all cases the unloaded edges of the composite plate are simply supported whereas those of the three-strip composite panel and five-strip composite panel are fi-ee. Displacement function comprises a quintic polynomial in the transverse direction and a 10-term Chebyshev polynomial in the longitudinal direction is chosen to model the out-of-plane deflection. Comparison is made against the displacement fiinction which use trigonometric function in the longitudinal direction. A FORTRAN program has been developed to generate the desired results. The validity of the results obtained are verified by comparing with published results. Geometric parametric studies such as the effect of flange width to web width ratio on the buckling behaviour of composite panels of plain channel and lipped channel shapes is illustrated. In addition, the effect of lip to flange ratio on the buckling behaviour of five-strip composite panel in the shape of lipped channel is also investigated. The advantage of using Chebyshev polynomial over trigonometric function is also discussed.
author2 Khong, Poh Wah
author_facet Khong, Poh Wah
Toh, Hoong Thiam.
format Theses and Dissertations
author Toh, Hoong Thiam.
author_sort Toh, Hoong Thiam.
title Stability study of composite panels
title_short Stability study of composite panels
title_full Stability study of composite panels
title_fullStr Stability study of composite panels
title_full_unstemmed Stability study of composite panels
title_sort stability study of composite panels
publishDate 2009
url http://hdl.handle.net/10356/19850
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