Stability of Composite and Sandwich Struts by Mixed Formulation

A unified mixed, higher-order analytical formulation is presented to evaluate the buckling of laminated composite struts. The formulation can also be used to evaluate the overall buckling and wrinkling loads of a general multilayer, multicore sandwich strut having any arbitrary sequence of stiff lay...

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Published inJournal of engineering mechanics Vol. 130; no. 7; pp. 762 - 770
Main Authors Dafedar, J. B, Desai, Y. M
Format Journal Article
LanguageEnglish
Published American Society of Civil Engineers 01.07.2004
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TECHNICAL PAPERS
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Abstract A unified mixed, higher-order analytical formulation is presented to evaluate the buckling of laminated composite struts. The formulation can also be used to evaluate the overall buckling and wrinkling loads of a general multilayer, multicore sandwich strut having any arbitrary sequence of stiff layers and cores. The usual assumptions of thin stiff layers and antiplane core are advantageously eliminated. Displacements as well as transverse stress continuities are enforced in the formulation by incorporating them as the degrees of freedom, thus avoiding separate calculations of the modal transverse stresses. Two sets of mixed models are proposed, based on individual layer and equivalent single layer theories, by selectively incorporating nonlinear components of Green's strain tensor. Limitations of the equivalent single-layer theories and typical simplifying assumptions are highlighted. A parametric investigation is presented, concerning the influence of the material and geometric properties on the buckling behavior of a sandwich strut. A few recommendations are also made for the stability analysis of laminated composite struts.
AbstractList A unified mixed, higher-order analytical formulation is presented to evaluate the buckling of laminated composite struts. The formulation can also be used to evaluate the overall buckling and wrinkling loads of a general multilayer, multicore sandwich strut having any arbitrary sequence of stiff layers and cores. The usual assumptions of thin stiff layers and antiplane core are advantageously eliminated. Displacements as well as transverse stress continuities are enforced in the formulation by incorporating them as the degrees of freedom, thus avoiding separate calculations of the modal transverse stresses. Two sets of mixed models are proposed, based on individual layer and equivalent single layer theories, by selectively incorporating nonlinear components of Green's strain tensor. Limitations of the equivalent single-layer theories and typical simplifying assumptions are highlighted. A parametric investigation is presented, concerning the influence of the material and geometric properties on the buckling behavior of a sandwich strut. A few recommendations are also made for the stability analysis of laminated composite struts.
Author Desai, Y. M
Dafedar, J. B
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Cites_doi 10.2514/3.10509
10.1177/073168449101000107
10.1061/(ASCE)0733-9399(1993)119:3(476)
10.2514/3.10202
10.1017/S0001924000029122
10.1016/S0263-8223(97)00048-2
10.2514/3.4054
10.1016/B978-0-08-012870-2.50006-7
10.1016/0020-7462(90)90006-U
10.1016/S0263-8223(00)00077-5
10.1016/0263-8223(95)00150-6
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References Reddy, J. N. 1990; 25
Khdeir, A. A.; Reddy, J. N. 1997; 37
Kapania, R. K.; Raciti, S. 1989; 27
Barbero, E. J.; Reddy, J. N. 1990; 28
Benson, A. S.; Mayers, J. 1967; 5
Kant, T.; Patil, H. S. 1991; 10
Webber, J. P. H.; Kyriakides, S.; Lee, C. T. 1976; 80
Frostig, Y.; Baruch, M. 1993; 119
Chattopadhyay, A.; Gu, H. 1996; 34
Hadi, B. K.; Matthews, F. L. 2000; 49
e_1_2_1_7_1
e_1_2_1_8_1
e_1_2_1_5_1
e_1_2_1_6_1
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e_1_2_1_4_1
e_1_2_1_10_1
e_1_2_1_2_1
e_1_2_1_11_1
Webber J. P. H. (e_1_2_1_12_1) 1976; 80
e_1_2_1_9_1
References_xml – volume: 25
  start-page: 677
  issn: 0020-7462
  year: 1990
  end-page: 686
  article-title: A general nonlinear third-order theory of plates with moderate thickness.
  publication-title: Int. J. Non-Linear Mech.
  contributor:
    fullname: Reddy, J. N.
– volume: 28
  start-page: 1987
  issn: 0001-1452
  year: 1990
  end-page: 1994
  article-title: Nonlinear analysis of composite laminates using a generalized laminated plate theory.
  publication-title: AIAA J.
  contributor:
    fullname: Barbero, E. J.; Reddy, J. N.
– volume: 37
  start-page: 1
  issn: 0263-8223
  year: 1997
  end-page: 3
  article-title: Buckling of cross-ply laminated beams with arbitrary boundary conditions.
  publication-title: Compos. Struct.
  contributor:
    fullname: Khdeir, A. A.; Reddy, J. N.
– volume: 119
  start-page: 476
  issn: 0733-9399
  year: 1993
  end-page: 495
  article-title: High-order buckling analysis of sandwich beams with transversely flexible core.
  publication-title: J. Eng. Mech.
  contributor:
    fullname: Frostig, Y.; Baruch, M.
– volume: 10
  start-page: 102
  issn: 0731-6844
  year: 1991
  end-page: 109
  article-title: Buckling loads of sandwich columns with a higher-order theory.
  publication-title: J. Reinf. Plast. Compos.
  contributor:
    fullname: Kant, T.; Patil, H. S.
– volume: 5
  start-page: 729
  issn: 0001-1452
  year: 1967
  end-page: 739
  article-title: General instability and face wrinkling of sandwich plates-unified theory and applications.
  publication-title: AIAA J.
  contributor:
    fullname: Benson, A. S.; Mayers, J.
– volume: 27
  start-page: 923
  issn: 0001-1452
  year: 1989
  end-page: 934
  article-title: Recent advances in analysis of laminated beams and plates. Part I: Shear effects and buckling.
  publication-title: AIAA J.
  contributor:
    fullname: Kapania, R. K.; Raciti, S.
– volume: 49
  start-page: 425
  issn: 0263-8223
  year: 2000
  end-page: 434
  article-title: Development of Benson-Mayer theory on the wrinkling of anisotropic sandwich panels.
  publication-title: Compos. Struct.
  contributor:
    fullname: Hadi, B. K.; Matthews, F. L.
– volume: 34
  start-page: 291
  issn: 0263-8223
  year: 1996
  end-page: 299
  article-title: Exact elasticity solution for buckling of composite laminates.
  publication-title: Compos. Struct.
  contributor:
    fullname: Chattopadhyay, A.; Gu, H.
– volume: 80
  start-page: 264
  issn: 0001-9240
  year: 1976
  end-page: 272
  article-title: On the wrinkling of honeycomb sandwich columns with laminated cross-ply faces.
  publication-title: Aeronaut. J.
  contributor:
    fullname: Webber, J. P. H.; Kyriakides, S.; Lee, C. T.
– ident: e_1_2_1_3_1
  doi: 10.2514/3.10509
– ident: e_1_2_1_8_1
  doi: 10.1177/073168449101000107
– ident: e_1_2_1_6_1
  doi: 10.1061/(ASCE)0733-9399(1993)119:3(476)
– ident: e_1_2_1_9_1
  doi: 10.2514/3.10202
– volume: 80
  start-page: 264
  year: 1976
  ident: e_1_2_1_12_1
  article-title: On the wrinkling of honeycomb sandwich columns with laminated cross-ply faces.
  publication-title: Aeronaut. J.
  doi: 10.1017/S0001924000029122
  contributor:
    fullname: Webber J. P. H.
– ident: e_1_2_1_10_1
  doi: 10.1016/S0263-8223(97)00048-2
– ident: e_1_2_1_4_1
  doi: 10.2514/3.4054
– ident: e_1_2_1_2_1
  doi: 10.1016/B978-0-08-012870-2.50006-7
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  doi: 10.1016/0020-7462(90)90006-U
– ident: e_1_2_1_7_1
  doi: 10.1016/S0263-8223(00)00077-5
– ident: e_1_2_1_5_1
  doi: 10.1016/0263-8223(95)00150-6
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Snippet A unified mixed, higher-order analytical formulation is presented to evaluate the buckling of laminated composite struts. The formulation can also be used to...
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Title Stability of Composite and Sandwich Struts by Mixed Formulation
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