A novel unified model for laminated composite beams
Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature....
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Nguyen, Trung-Kien [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2020transfer abstract |
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| Schlagwörter: |
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| Übergeordnetes Werk: |
Enthalten in: Versatile, but not focused, traffic offenders are more likely to be at fault for a fatal crash - Davey, Benjamin ELSEVIER, 2022, an international journal, Amsterdam |
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| Übergeordnetes Werk: |
volume:238 ; year:2020 ; day:15 ; month:04 ; pages:0 |
| Links: |
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| DOI / URN: |
10.1016/j.compstruct.2020.111943 |
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| Katalog-ID: |
ELV049504134 |
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| 520 | |a Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. | ||
| 520 | |a Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. | ||
| 650 | 7 | |a Vibration |2 Elsevier | |
| 650 | 7 | |a Bending |2 Elsevier | |
| 650 | 7 | |a Shear deformation beam theory |2 Elsevier | |
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10.1016/j.compstruct.2020.111943 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000000926.pica (DE-627)ELV049504134 (ELSEVIER)S0263-8223(19)33829-2 DE-627 ger DE-627 rakwb eng 690 VZ 50.17 bkl 55.80 bkl 44.80 bkl Nguyen, Trung-Kien verfasserin aut A novel unified model for laminated composite beams 2020transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Vibration Elsevier Bending Elsevier Shear deformation beam theory Elsevier Laminated composite beam Elsevier Buckling Elsevier Nguyen, Ba-Duy oth Vo, Thuc P. oth Thai, Huu-Tai oth Enthalten in Elsevier Davey, Benjamin ELSEVIER Versatile, but not focused, traffic offenders are more likely to be at fault for a fatal crash 2022 an international journal Amsterdam (DE-627)ELV007891687 volume:238 year:2020 day:15 month:04 pages:0 https://doi.org/10.1016/j.compstruct.2020.111943 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 50.17 Sicherheitstechnik VZ 55.80 Verkehrswesen Transportwesen: Allgemeines VZ 44.80 Unfallmedizin Notfallmedizin VZ AR 238 2020 15 0415 0 |
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10.1016/j.compstruct.2020.111943 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000000926.pica (DE-627)ELV049504134 (ELSEVIER)S0263-8223(19)33829-2 DE-627 ger DE-627 rakwb eng 690 VZ 50.17 bkl 55.80 bkl 44.80 bkl Nguyen, Trung-Kien verfasserin aut A novel unified model for laminated composite beams 2020transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Vibration Elsevier Bending Elsevier Shear deformation beam theory Elsevier Laminated composite beam Elsevier Buckling Elsevier Nguyen, Ba-Duy oth Vo, Thuc P. oth Thai, Huu-Tai oth Enthalten in Elsevier Davey, Benjamin ELSEVIER Versatile, but not focused, traffic offenders are more likely to be at fault for a fatal crash 2022 an international journal Amsterdam (DE-627)ELV007891687 volume:238 year:2020 day:15 month:04 pages:0 https://doi.org/10.1016/j.compstruct.2020.111943 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 50.17 Sicherheitstechnik VZ 55.80 Verkehrswesen Transportwesen: Allgemeines VZ 44.80 Unfallmedizin Notfallmedizin VZ AR 238 2020 15 0415 0 |
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10.1016/j.compstruct.2020.111943 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000000926.pica (DE-627)ELV049504134 (ELSEVIER)S0263-8223(19)33829-2 DE-627 ger DE-627 rakwb eng 690 VZ 50.17 bkl 55.80 bkl 44.80 bkl Nguyen, Trung-Kien verfasserin aut A novel unified model for laminated composite beams 2020transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Vibration Elsevier Bending Elsevier Shear deformation beam theory Elsevier Laminated composite beam Elsevier Buckling Elsevier Nguyen, Ba-Duy oth Vo, Thuc P. oth Thai, Huu-Tai oth Enthalten in Elsevier Davey, Benjamin ELSEVIER Versatile, but not focused, traffic offenders are more likely to be at fault for a fatal crash 2022 an international journal Amsterdam (DE-627)ELV007891687 volume:238 year:2020 day:15 month:04 pages:0 https://doi.org/10.1016/j.compstruct.2020.111943 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 50.17 Sicherheitstechnik VZ 55.80 Verkehrswesen Transportwesen: Allgemeines VZ 44.80 Unfallmedizin Notfallmedizin VZ AR 238 2020 15 0415 0 |
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10.1016/j.compstruct.2020.111943 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000000926.pica (DE-627)ELV049504134 (ELSEVIER)S0263-8223(19)33829-2 DE-627 ger DE-627 rakwb eng 690 VZ 50.17 bkl 55.80 bkl 44.80 bkl Nguyen, Trung-Kien verfasserin aut A novel unified model for laminated composite beams 2020transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Vibration Elsevier Bending Elsevier Shear deformation beam theory Elsevier Laminated composite beam Elsevier Buckling Elsevier Nguyen, Ba-Duy oth Vo, Thuc P. oth Thai, Huu-Tai oth Enthalten in Elsevier Davey, Benjamin ELSEVIER Versatile, but not focused, traffic offenders are more likely to be at fault for a fatal crash 2022 an international journal Amsterdam (DE-627)ELV007891687 volume:238 year:2020 day:15 month:04 pages:0 https://doi.org/10.1016/j.compstruct.2020.111943 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 50.17 Sicherheitstechnik VZ 55.80 Verkehrswesen Transportwesen: Allgemeines VZ 44.80 Unfallmedizin Notfallmedizin VZ AR 238 2020 15 0415 0 |
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10.1016/j.compstruct.2020.111943 doi /cbs_pica/cbs_olc/import_discovery/elsevier/einzuspielen/GBV00000000000926.pica (DE-627)ELV049504134 (ELSEVIER)S0263-8223(19)33829-2 DE-627 ger DE-627 rakwb eng 690 VZ 50.17 bkl 55.80 bkl 44.80 bkl Nguyen, Trung-Kien verfasserin aut A novel unified model for laminated composite beams 2020transfer abstract nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. Vibration Elsevier Bending Elsevier Shear deformation beam theory Elsevier Laminated composite beam Elsevier Buckling Elsevier Nguyen, Ba-Duy oth Vo, Thuc P. oth Thai, Huu-Tai oth Enthalten in Elsevier Davey, Benjamin ELSEVIER Versatile, but not focused, traffic offenders are more likely to be at fault for a fatal crash 2022 an international journal Amsterdam (DE-627)ELV007891687 volume:238 year:2020 day:15 month:04 pages:0 https://doi.org/10.1016/j.compstruct.2020.111943 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U 50.17 Sicherheitstechnik VZ 55.80 Verkehrswesen Transportwesen: Allgemeines VZ 44.80 Unfallmedizin Notfallmedizin VZ AR 238 2020 15 0415 0 |
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Nguyen, Trung-Kien |
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a novel unified model for laminated composite beams |
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A novel unified model for laminated composite beams |
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Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. |
| abstractGer |
Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. |
| abstract_unstemmed |
Based on fundamental equations of the elasticity theory, a novel unified beam model is developed for laminated composite beams. In this model, the displacement field is selected in a unified form which can be recovered to that of existing shear deformation beam theories available in the literature. Based on Lagrange’s equations, the governing equations of the present theory are derived. They are then solved for deflections, stresses, natural frequencies and critical buckling loads of composite beams under different boundary conditions and lay-ups by using the Ritz approach with novel hybrid trigonometric functions. Various examples are also presented to verify the accuracy and generalization of the present theory, as well as investigate the influences of fibre angle on the behaviour of composite beams under different boundary conditions and lay-ups. |
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A novel unified model for laminated composite beams |
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Nguyen, Ba-Duy Vo, Thuc P. Thai, Huu-Tai |
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