Assessment of Composite and Sandwich Laminates Using a New Shear Deformation Theory

复合材料层合板 复合数 材料科学 剪切(地质) 复合材料 结构工程 变形(气象学) 工程类
作者
Suganyadevi Sarangan,B.N. Singh
出处
期刊:AIAA Journal [American Institute of Aeronautics and Astronautics]
卷期号:54 (2): 789-792 被引量:18
标识
DOI:10.2514/1.j054443
摘要

No AccessTechnical NoteAssessment of Composite and Sandwich Laminates Using a New Shear Deformation TheoryS. Suganyadevi and B. N. SinghS. SuganyadeviIndian Institute of Technology, Kharagpur 721 302, India and B. N. SinghIndian Institute of Technology, Kharagpur 721 302, IndiaPublished Online:29 Dec 2015https://doi.org/10.2514/1.J054443SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Kant T. and Swaminathan K., “Analytical Solutions for Free Vibration of Laminated Composite and Sandwich Plates Based on a Higher-Order Refined Theory,” Composite Structures, Vol. 53, No. 12, July 2001, pp. 73–85. doi:https://doi.org/10.1016/S0263-8223(00)00180-X COMSE2 0263-8223 CrossrefGoogle Scholar[2] Aydogdu M., “A New Shear Deformation Theory for Laminated Composite Plates,” Composite Structures, Vol. 89, No. 12, June 2009, pp. 94–101. doi:https://doi.org/10.1016/j.compstruct.2008.07.008 COMSE2 0263-8223 CrossrefGoogle Scholar[3] Pagano N. J., “Exact Solutions for Rectangular Bidirectional Composites and Sandwich Plates,” Journal of Composite Materials, Vol. 4, No. 12, 1970, pp. 20–34. doi:https://doi.org/10.1177/002199837000400102 CMMTBM 0095-4497 Google Scholar[4] Grover N., Singh B. N. and Maiti D. K., “New Nonpolynomial Shear-Deformation Theories for Structural Behavior of Laminated-Composite and Sandwich Plates,” AIAA Journal, Vol. 51, No. 8, Aug. 2013, pp. 1861–1871. doi:https://doi.org/10.2514/1.J052399 AIAJAH 0001-1452 LinkGoogle Scholar[5] Di Sciuva M., “Bending, Vibration and Buckling of Simply Supported Thick Multilayered Orthotropic Plates: An Evaluation of a New Displacement Model,” Journal of Sound and Vibration, Vol. 105, No. 3, March 1986, pp. 425–442. doi:https://doi.org/10.1016/0022-460X(86)90169-0 JSVIAG 0022-460X CrossrefGoogle Scholar[6] Srinivas S. and Rao A. K., “Bending, Vibration and Buckling of Simply Supported Thick Orthotropic Rectangular Plates and Laminates,” International Journal of Solids and Structures, Vol. 6, No. 11, Nov. 1970, pp. 1463–1481. doi:https://doi.org/10.1016/0020-7683(70)90076-4 IJSOAD 0020-7683 CrossrefGoogle Scholar[7] Karama M., Afaq K. S. and Mistou S., “A New Theory for Laminated Composite Plates,” Journal of Materials: Design and Applications, Vol. 223, No. 2, April 2009, pp. 53–62. doi:https://doi.org/10.1243/14644207JMDA189 Google Scholar[8] Reddy J. N., “A Simple Higher-Order Theory for Laminated Composite Plates,” Journal of Applied Mechanics, Vol. 51, No. 4, 1984, pp. 745–752. doi:https://doi.org/10.1115/1.3167719 JAMCAV 0021-8936 CrossrefGoogle Scholar[9] Pagano N. J. and Hatifield H. J., “Elastic Behavior of Multilayered Bidirectional Composites,” AIAA Journal, Vol. 10, No. 7, July 1972, pp. 931–933. doi:https://doi.org/10.2514/3.50249 AIAJAH 0001-1452 LinkGoogle Scholar[10] Kulkarni S. D. and Kapuria S., “Free Vibration Analysis of Composite and Sandwich Plates Using an Improved Discrete Kirchhoff Quadrilateral Element Based on Third-Order Zigzag Theory,” Computational Mechanics, Vol. 42, No. 6, April 2008, pp. 803–824. doi:https://doi.org/10.1007/s00466-008-0285-z CMADEJ CrossrefGoogle Scholar[11] Putcha N. S. and Reddy J. N., “Stability and Natural Vibration Analysis of Laminated Plates by Using a Mixed Element Based on a Refined Plate Theory,” Journal of Sound and Vibration, Vol. 104, No. 2, Jan. 1986, pp. 285–300. doi:https://doi.org/10.1016/0022-460X(86)90269-5 JSVIAG 0022-460X CrossrefGoogle Scholar[12] Noor A. K., “Stability of Multilayered Composite Plates,” Fibre Science and Technology, Vol. 8, No. 2, April 1975, pp. 81–89. doi:https://doi.org/10.1016/0015-0568(75)90005-6 FSTEBJ 0015-0568 CrossrefGoogle Scholar[13] Srinivas S., “A Refined Analysis of Composite Laminates,” Journal of Sound and Vibration, Vol. 30, No. 4, Oct. 1973, pp. 495–507. doi:https://doi.org/10.1016/S0022-460X(73)80170-1 JSVIAG 0022-460X CrossrefGoogle Scholar Previous article Next article

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