Application of a three-dimensional mixed finite element model to the flexure of sandwich plate
The bending analysis of sandwich plates consisting of very stiff face sheets and a comparatively flexible core material offers challenge due to large variation in the magnitude of stress and strain components in the face and in the core regions of the plate. Similarly, the displacement fields do var...
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Published in | Computers & structures Vol. 81; no. 22; pp. 2183 - 2198 |
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Main Authors | , , |
Format | Journal Article |
Language | English |
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Elsevier Ltd
01.09.2003
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Abstract | The bending analysis of sandwich plates consisting of very stiff face sheets and a comparatively flexible core material offers challenge due to large variation in the magnitude of stress and strain components in the face and in the core regions of the plate. Similarly, the displacement fields do vary in zigzag manner at the layer interface of stiff face sheet and the soft core, thereby making the transverse strains highly discontinuous at such layer interfaces. All these behavioural aspects indicate that only an individual layerwise model can appropriately analyze sandwich plates. A layerwise (three-dimensional), mixed, 18-node finite element (FE) model developed by Ramtekkar et al. [Mech. Adv. Mater. Struct. 9 (2002) 133] has been employed for the accurate evaluation of transverse stresses in sandwich laminates. The FE model consists of six degrees-of-freedom (three displacement components and three transverse stress components
τ
xz
,
τ
yz
,
σ
z
, where
z is the thickness direction) per node which ensures the through thickness continuity of transverse stress and displacement fields. Results obtained by using the FE model have shown excellent agreement with the available elasticity solutions for sandwich plates. Additional results on the variation of transverse strains have also been presented to highlight the magnitude of discontinuity in these quantities due to difference in properties of the face and the core materials of sandwich plates. |
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AbstractList | The bending analysis of sandwich plates consisting of very stiff face sheets and a comparatively flexible core material offers challenge due to large variation in the magnitude of stress and strain components in the face and in the core regions of the plate. Similarly, the displacement fields do vary in zigzag manner at the layer interface of stiff face sheet and the soft core, thereby making the transverse strains highly discontinuous at such layer interfaces. All these behavioural aspects indicate that only an individual layerwise model can appropriately analyze sandwich plates. A layerwise (three-dimensional), mixed, 18-node finite element (FE) model developed by Ramtekkar et al. [Mech. Adv. Mater. Struct. 9 (2002) 133] has been employed for the accurate evaluation of transverse stresses in sandwich laminates. The FE model consists of six degrees-of-freedom (three displacement components and three transverse stress components *txz, *tyz, *sz where z is the thickness direction) per node which ensures the through thickness continuity of transverse stress and displacement fields. Results obtained by using the FE model have shown excellent agreement with the available elasticity solutions for sandwich plates. Additional results on the variation of transverse strains have also been presented to highlight the magnitude of discontinuity in these quantities due to difference in properties of the face and the core materials of sandwich plates. The bending analysis of sandwich plates consisting of very stiff face sheets and a comparatively flexible core material offers challenge due to large variation in the magnitude of stress and strain components in the face and in the core regions of the plate. Similarly, the displacement fields do vary in zigzag manner at the layer interface of stiff face sheet and the soft core, thereby making the transverse strains highly discontinuous at such layer interfaces. All these behavioural aspects indicate that only an individual layerwise model can appropriately analyze sandwich plates. A layerwise (three-dimensional), mixed, 18-node finite element (FE) model developed by Ramtekkar et al. [Mech. Adv. Mater. Struct. 9 (2002) 133] has been employed for the accurate evaluation of transverse stresses in sandwich laminates. The FE model consists of six degrees-of-freedom (three displacement components and three transverse stress components τ xz , τ yz , σ z , where z is the thickness direction) per node which ensures the through thickness continuity of transverse stress and displacement fields. Results obtained by using the FE model have shown excellent agreement with the available elasticity solutions for sandwich plates. Additional results on the variation of transverse strains have also been presented to highlight the magnitude of discontinuity in these quantities due to difference in properties of the face and the core materials of sandwich plates. |
Author | Ramtekkar, G.S. Desai, Y.M. Shah, A.H. |
Author_xml | – sequence: 1 givenname: G.S. surname: Ramtekkar fullname: Ramtekkar, G.S. organization: Department of Civil Engineering, Govt. Engineering College Raipur, Raipur (C.G.) 492010, India – sequence: 2 givenname: Y.M. surname: Desai fullname: Desai, Y.M. email: desai@civil.iitb.ac.in organization: Department of Civil Engineering, Indian Institute of Technology Bombay, Powai, Mumbai 400076, India – sequence: 3 givenname: A.H. surname: Shah fullname: Shah, A.H. organization: Department of Civil Engineering, The University of Manitoba, Winnipeg, Man., Canada R3T 2N2 |
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Cites_doi | 10.1016/0020-7683(88)90090-X 10.1016/0029-5493(81)90001-7 10.1002/(SICI)1097-0207(19960615)39:11<1797::AID-NME928>3.0.CO;2-W 10.1016/0263-8223(93)90191-R 10.1002/nme.1620200315 10.1177/002199839102500803 10.1115/1.3423688 10.1002/cnm.1630030303 10.1016/0263-8223(92)90019-9 10.1016/S0263-8223(98)00097-X 10.1080/153764902753510516 10.1002/nme.1620362209 10.1016/0263-8223(93)90052-R 10.1108/eb023922 10.2514/3.10765 10.1016/0263-8223(92)90026-9 10.1177/002199837000400102 10.1115/1.2791769 10.1016/0020-7683(70)90076-4 10.1016/0045-7949(94)90005-1 10.1016/0263-8223(93)90187-U |
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Struct. doi: 10.1080/153764902753510516 contributor: fullname: Ramtekkar – volume: 36 start-page: 3909 year: 1993 ident: 10.1016/S0045-7949(03)00289-X_BIB3 article-title: A three-dimensional multilayer composite finite element for stress analysis of composite laminates publication-title: Int. J. Numer. Meth. Eng. doi: 10.1002/nme.1620362209 contributor: fullname: Han – volume: 24 start-page: 29 year: 1993 ident: 10.1016/S0045-7949(03)00289-X_BIB9 article-title: An interlaminar stress mixed finite element method for the analysis of thick laminated composite plates publication-title: Compos. Struct. doi: 10.1016/0263-8223(93)90052-R contributor: fullname: Wu – volume: 10 start-page: 499 year: 1993 ident: 10.1016/S0045-7949(03)00289-X_BIB21 article-title: On evaluation of transverse stresses in layered symmetric composite and sandwich laminates under flexure publication-title: Eng. Comput. doi: 10.1108/eb023922 contributor: fullname: Manjunatha – volume: 29 start-page: 1498 issue: 9 year: 1991 ident: 10.1016/S0045-7949(03)00289-X_BIB12 article-title: Analysis of sandwich plates using a hybrid-stress finite element publication-title: AIAA J. doi: 10.2514/3.10765 contributor: fullname: Rao – volume: 20 start-page: 195 year: 1992 ident: 10.1016/S0045-7949(03)00289-X_BIB8 article-title: A general laminated plate theory accounting for continuity of displacements and transverse shear stresses at material interfaces publication-title: Compos. Struct. doi: 10.1016/0263-8223(92)90026-9 contributor: fullname: Soldatos – volume: 4 start-page: 20 year: 1970 ident: 10.1016/S0045-7949(03)00289-X_BIB6 article-title: Exact solutions for rectangular bi-directional composites and sandwich plates publication-title: J. Compos. Mater. doi: 10.1177/002199837000400102 contributor: fullname: Pagano – volume: 66 start-page: 1004 year: 1999 ident: 10.1016/S0045-7949(03)00289-X_BIB18 article-title: Transverse normal stress effects in multilayered plates publication-title: ASME J. Appl. Mech. doi: 10.1115/1.2791769 contributor: fullname: Carrera – volume: 6 start-page: 1463 year: 1970 ident: 10.1016/S0045-7949(03)00289-X_BIB5 article-title: Bending vibration and buckling of simply supported thick orthotropic rectangular plates and laminates publication-title: Int. J. Solids Struct. doi: 10.1016/0020-7683(70)90076-4 contributor: fullname: Srinivas – volume: 50 start-page: 351 issue: 3 year: 1994 ident: 10.1016/S0045-7949(03)00289-X_BIB22 article-title: On accurate estimation of transverse stresses in multilayer laminates publication-title: Comput. Struct. doi: 10.1016/0045-7949(94)90005-1 contributor: fullname: Kant – volume: 25 start-page: 397 year: 1993 ident: 10.1016/S0045-7949(03)00289-X_BIB14 article-title: Analysis of sandwich plates using mixed finite element publication-title: Compos. Struct. doi: 10.1016/0263-8223(93)90187-U contributor: fullname: Wu |
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Title | Application of a three-dimensional mixed finite element model to the flexure of sandwich plate |
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