Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression
A buckling analysis has been carried out to investigate the response of laminated composite cylindrical panel with an elliptical cutout subject to axial loading. The numerical analysis was performed using the Abaqus finite-element software. The effect of the location and size of the cutout and also...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2012-01-01
|
| Series: | Modelling and Simulation in Engineering |
| Online Access: | http://dx.doi.org/10.1155/2012/171953 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832568309897232384 |
|---|---|
| author | Hamidreza Allahbakhsh Ali Dadrasi |
| author_facet | Hamidreza Allahbakhsh Ali Dadrasi |
| author_sort | Hamidreza Allahbakhsh |
| collection | DOAJ |
| description | A buckling analysis has been carried out to investigate the response of laminated composite cylindrical panel with an elliptical cutout subject to axial loading. The numerical analysis was performed using the Abaqus finite-element software. The effect of the location and size of the cutout and also the composite ply angle on the buckling load of laminated composite cylindrical panel is investigated. Finally, simple equations, in the form of a buckling load reduction factor, were presented by using the least square regression method. The results give useful information into designing a laminated composite cylindrical panel, which can be used to improve the load capacity of cylindrical panels. |
| format | Article |
| id | doaj-art-aea30594e47b4005b7cd95c634ea9630 |
| institution | Kabale University |
| issn | 1687-5591 1687-5605 |
| language | English |
| publishDate | 2012-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Modelling and Simulation in Engineering |
| spelling | doaj-art-aea30594e47b4005b7cd95c634ea96302025-02-03T00:59:19ZengWileyModelling and Simulation in Engineering1687-55911687-56052012-01-01201210.1155/2012/171953171953Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial CompressionHamidreza Allahbakhsh0Ali Dadrasi1Mechanical Department, Islamic Azad University, Shahrood Branch, Shahrood, IranMechanical Department, Islamic Azad University, Shahrood Branch, Shahrood, IranA buckling analysis has been carried out to investigate the response of laminated composite cylindrical panel with an elliptical cutout subject to axial loading. The numerical analysis was performed using the Abaqus finite-element software. The effect of the location and size of the cutout and also the composite ply angle on the buckling load of laminated composite cylindrical panel is investigated. Finally, simple equations, in the form of a buckling load reduction factor, were presented by using the least square regression method. The results give useful information into designing a laminated composite cylindrical panel, which can be used to improve the load capacity of cylindrical panels.http://dx.doi.org/10.1155/2012/171953 |
| spellingShingle | Hamidreza Allahbakhsh Ali Dadrasi Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression Modelling and Simulation in Engineering |
| title | Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression |
| title_full | Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression |
| title_fullStr | Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression |
| title_full_unstemmed | Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression |
| title_short | Buckling Analysis of Laminated Composite Panel with Elliptical Cutout Subject to Axial Compression |
| title_sort | buckling analysis of laminated composite panel with elliptical cutout subject to axial compression |
| url | http://dx.doi.org/10.1155/2012/171953 |
| work_keys_str_mv | AT hamidrezaallahbakhsh bucklinganalysisoflaminatedcompositepanelwithellipticalcutoutsubjecttoaxialcompression AT alidadrasi bucklinganalysisoflaminatedcompositepanelwithellipticalcutoutsubjecttoaxialcompression |