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TECHNICAL PAPERS

Higher-Order Zig-Zag Theory for Laminated Composites With Multiple Delaminations

[+] Author and Article Information
M. Cho

School of Mechanical and Aerospace Engineering, Seoul National University, Seoul 151-742, Korea   e-mail: mhcho@snu.ac.kr

J.-S. Kim

Department of Aerospace Engineering, Inha University, Inchon 402-751, Korea

J. Appl. Mech 68(6), 869-877 (Oct 19, 2000) (9 pages) doi:10.1115/1.1406959 History: Received July 12, 1999; Revised October 19, 2000
Copyright © 2001 by ASME
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References

Lo,  K. H., Christensen,  R. M., and Wu,  E. M., 1977, “A Higher-Order Theory of Plate Deformation, Part 2: Laminated Plates,” ASME J. Appl. Mech., 44, pp. 669–676.
Reddy,  J. N., 1987, “A Generalization of Two-Dimensional Theories of Laminated Plates,” Commun. Appl. Numer. Methods, 3, pp. 173–180.
Di Sciuva,  M., 1986, “Bending, Vibration and Buckling of Simply Supported Thick Multilayered Orthotropic Plates: An Evaluation of a New Displacement Model,” J. Sound Vib., 105, pp. 425–442.
Noor,  A. K., and Burton,  W. S., 1989, “Assessment of Shear Deformation Theories for Multilayered Composite Plates,” Appl. Mech. Rev., 42, pp. 1–13.
Kapania,  R. K., and Raciti,  S., 1989, “Recent Advanced in Analysis of Laminated Beams and Plates,” AIAA J., 27, pp. 923–946.
Reddy,  J. N., and Robbins,  D. H. 1994, “Theories and Computational Models for Composite Laminates,” Appl. Mech. Rev., 47, pp. 147–169.
Simitses, G. J., 1995, “Delamination Buckling of Flat Laminates,” Buckling and Postbuckling of Composite Plates, G. J. Turvey and I. H. Marshall, eds., Chapman & Hall, London, pp. 299–328.
Wang,  J. T. S., Liu,  Y. Y., and Gibby,  J. A., 1982, “Vibrations of Split Beams,” J. Sound Vib., 84, pp. 491–502.
Wang, J. T. S., and Lin, C. C., 1995, “Vibration of Beam-Plates Having Multiple Delaminations,” Proceedings of the AIAA/ASME/ASCE/AHS/ASC 36th Structures, Structural Dynamics and Materials Conference, New Orleans, LA, AIAA, Reston, VA, pp. 3126–3133.
Shen,  M.-H. H., and Grady,  J. E., 1992, “Free Vibration of Delaminated Beams,” AIAA J., 30, pp. 1361–1370.
Gummadi, L. N. B., and Hanagud, S., 1995, “Vibration Characteristics of Beams With Multiple Delaminations,” Proceedings of the AIAA/ASME/ASCE/AHS/ASC 36th Structures, Structural Dynamics and Materials Conference, New Orleans, LA, AIAA, Reston, VA, pp. 140–150.
Chattopadhyay,  A., Dragomir-Daescu,  D., and Gu,  H., 1999, “Dynamics of Delaminated Smart Composite Cross-Ply Beams,” Smart Mater. Struct., 8, pp. 92–99.
Seeley,  C. E., and Chattopadhyay,  A., 1999, “Modeling of Adaptive Composites Including Debonding,” Int. J. Solids Struct., 36, pp. 1823–1843.
Islam,  A. S., and Craig,  K. C., 1994, “Damage Detection in Composite Structures Using Piezoelectric Materials,” Smart Mater. Struct., 3, pp. 318–328.
Lee,  J., Gürdal,  Z., and Griffin,  O. H., 1993, “Layer-Wise Approach for the Bifurcation Problem in Laminated Composites With Delaminations,” AIAA J., 31, pp. 331–338.
Cho,  M., and Kim,  J.-S., 1997, “Bifurcation Buckling Analysis of Delaminated Composites Using Global-Local Approach,” AIAA J., 35, pp. 1673–1676.
Cho, M., and Lee, S.-G., 1998, “Global/Local Analysis of Laminated Composites With Multiple Delaminations of Various Shapes,” Proceedings of the AIAA/ASME/ASCE/AHS/ASC 39th Structures, Structural Dynamics and Materials Conference, Long Beach, CA, AIAA, Reston, VA, pp. 76–86.
Kim,  J.-S., and Cho,  M., 1999, “Postbuckling of Delaminated Composites Under Compressive Loads Using Global-Local Approach,” AIAA J., 37, pp. 774–777.
Cheng,  Z-q., Jemah,  A. K., and Williams,  F. W., 1996, “Theory for Multilayered Anisotropic Plates With Weakened Interfaces,” ASME J. Appl. Mech., 63, pp. 1019–1026.
Di Sciuva,  M., 1997, “Geometrically Nonlinear Theory of Multilayered Plates With Interlayer Slips,” AIAA J., 35, pp. 1753–1759.
Chattopadhyay,  A., and Gu,  H., 1994, “New Higher Order Theory in Modeling Delamination Buckling of Composite Laminates,” AIAA J., 32, pp. 1709–1716.
Cho,  M., and Parmerter,  R. R., 1992, “An Efficient Higher-Order Plate Theory for Laminated Composites,” Composite Structures, 20, pp. 113–123.
Cho,  M., and Parmerter,  R. R., 1993, “Efficient Higher Order Composite Plate Theory for General Lamination Configurations,” AIAA J., 31, pp. 1299–1306.
Simitses,  G. J., Sallam,  S., and Yin,  W. L., 1985, “Effect of Delamination of Axially Loaded Homogeneous Laminated Plates,” AIAA J., 23, pp. 1437–1444.
Chen,  H. P., 1991, “Shear Deformation Theory for Compressive Delamination Buckling and Growth,” AIAA J., 29, pp. 813–819.
Gu,  H., and Chattopadhyay,  A., 1998, “Elasticity Approach for Delamination Buckling of Composite Beam Plates,” AIAA J., 36, pp. 2543–2551.

Figures

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Geometry of laminated composite with multiple delaminations
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Laminate deformed configurations with multiple delaminations
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Configuration of a simply supported beam-plate with a single delamination
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Nondimensionalized buckling load versus delamination length
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Configuration of a clamped beam-plate with centrally located delaminations
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Normalized buckling load versus delamination length for [0//90/90/0] composite, symmetric mode
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Normalized buckling load versus delamination length for [0//90/90/0] composite, antisymmetric mode
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Normalized buckling load versus delamination length for [0//90/0/90] composite
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Normalized buckling load versus delamination length for [0/90/90/0] composite with S=20, symmetric mode
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Normalized buckling load versus delamination length for [0/90/90/0] composite with S=20, antisymmetric mode
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Configuration of cantilevered [0/90]2s composite beam with a single delamination
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Configuration of cantilevered [0/90/90/0] composite beam with multiple delaminations
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Normalized natural frequency versus normalized distance for [0/90/90/0] composite with S=400
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Normalized natural frequency versus normalized distance for [0/90/90/0] composite with S=50
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Normalized natural frequency versus normalized distance for [0/90/90/0] composite with S=10

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