A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load
In this study, a thermal buckling analysis of laminate composite square plate was performed with elliptical hole cutout using the finite element method. Graphite/Epoxy laminate plate used in this study is symmetrical stacking sequence plate [(0/90)2]s. This laminate square plate was subjected to tem...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
De Gruyter
2020-06-01
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| Series: | Science and Engineering of Composite Materials |
| Subjects: | |
| Online Access: | https://doi.org/10.1515/secm-2020-0019 |
| _version_ | 1819148294244270080 |
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| author | Chhorn Buntheng Jung WooYoung |
| author_facet | Chhorn Buntheng Jung WooYoung |
| author_sort | Chhorn Buntheng |
| collection | DOAJ |
| description | In this study, a thermal buckling analysis of laminate composite square plate was performed with elliptical hole cutout using the finite element method. Graphite/Epoxy laminate plate used in this study is symmetrical stacking sequence plate [(0/90)2]s. This laminate square plate was subjected to temperature loading with clamped support on all edges. Moreover, the parameters considered were fiber orientation (θ), a/b ratio (elliptical hole), elliptical hole inclination (φ), thermal expansion coefficient ratio (α1/α2), and thickness of plates (t). The results showed that as the thermal expansion coefficient ratio changes, the elliptical hole ratio and the elliptical hole inclination have inconsequential effects on the performance of the resistance of laminate composite plates. The maximum values of thermal buckling amplification factor were obtained when the ratio a/b = 1.0, which is a circle cutout,while the minimum values were obtained when the ratio a/b = 0.5, regardless of the thickness of plates. Moreover, the plate with elliptical or circle cutout hole provides about 4% to 9% higher buckling resistance than that of the plate without hole cutout, because when subjected to temperature loading the plate with hole can release stress better than the plate without hole. |
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| id | doaj.art-f3e8984cca50408c96560e4f171509e4 |
| institution | Directory Open Access Journal |
| issn | 0792-1233 2191-0359 |
| language | English |
| last_indexed | 2024-12-22T13:43:25Z |
| publishDate | 2020-06-01 |
| publisher | De Gruyter |
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| series | Science and Engineering of Composite Materials |
| spelling | doaj.art-f3e8984cca50408c96560e4f171509e42022-12-21T18:23:52ZengDe GruyterScience and Engineering of Composite Materials0792-12332191-03592020-06-0127119620310.1515/secm-2020-0019secm-2020-0019A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling LoadChhorn Buntheng0Jung WooYoung1Gangneung-Wonju National University, College of Engineering, Building No. 2, Room 128, Gangneung city, Gangwon province [25457], KoreaGangneung-Wonju National University, College of Engineering, Building No. 2, Room 110, Gangneung city, Gangwon province [25457], KoreaIn this study, a thermal buckling analysis of laminate composite square plate was performed with elliptical hole cutout using the finite element method. Graphite/Epoxy laminate plate used in this study is symmetrical stacking sequence plate [(0/90)2]s. This laminate square plate was subjected to temperature loading with clamped support on all edges. Moreover, the parameters considered were fiber orientation (θ), a/b ratio (elliptical hole), elliptical hole inclination (φ), thermal expansion coefficient ratio (α1/α2), and thickness of plates (t). The results showed that as the thermal expansion coefficient ratio changes, the elliptical hole ratio and the elliptical hole inclination have inconsequential effects on the performance of the resistance of laminate composite plates. The maximum values of thermal buckling amplification factor were obtained when the ratio a/b = 1.0, which is a circle cutout,while the minimum values were obtained when the ratio a/b = 0.5, regardless of the thickness of plates. Moreover, the plate with elliptical or circle cutout hole provides about 4% to 9% higher buckling resistance than that of the plate without hole cutout, because when subjected to temperature loading the plate with hole can release stress better than the plate without hole.https://doi.org/10.1515/secm-2020-0019thermal bucklinglaminate compositeelliptical holefem |
| spellingShingle | Chhorn Buntheng Jung WooYoung A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load Science and Engineering of Composite Materials thermal buckling laminate composite elliptical hole fem |
| title | A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load |
| title_full | A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load |
| title_fullStr | A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load |
| title_full_unstemmed | A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load |
| title_short | A Parametric Study on the Elliptical hole Effects of Laminate Composite Plates under Thermal Buckling Load |
| title_sort | parametric study on the elliptical hole effects of laminate composite plates under thermal buckling load |
| topic | thermal buckling laminate composite elliptical hole fem |
| url | https://doi.org/10.1515/secm-2020-0019 |
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