Structural Engineering and Mechanics

  • 제13권6호
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  • Pages.695-711
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  • 2002
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  • 1225-4568(pISSN)
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  • 1598-6217(eISSN)
테크노프레스 (Techno-Press)
권호 표지
DOI QR코드

DOI QR Code

Comparative dynamic studies of thick laminated composite shells based on higher-order theories

  • Ganapathi, M. (Institute of Armament Technology) ;
  • Patel, B.P. (Institute of Armament Technology) ;
  • Pawargi, D.S. (Institute of Armament Technology) ;
  • Patel, H.G. (Institute of Armament Technology)
  • 투고 : 2001.11.19
  • 심사 : 2002.03.05
  • 발행 : 2002.06.25
⟨ 이전 논문 다음 논문 ⟩

초록

Here, the dynamic response characteristics of thick cross-ply laminated composite cylindrical shells are studied using a higher-order displacement model. The formulation accounts for the nonlinear variation of the in-plane and transverse displacements through the thickness, and abrupt discontinuity in slope of the in-plane displacements at any interface. The effect of inplane and rotary inertia terms is included. The analysis is carried out using finite element approach. The influences of various terms in the higher-order displacement field on the free vibrations, and transient dynamic response characteristics of cylindrical composite shells subjected to thermal and mechanical loads are analyzed.

키워드

참고문헌

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피인용 문헌

  1. Application of higher-order finite element for elastic stability analysis of laminated cross-ply oval cylindrical shells vol.40, pp.9-10, 2004, https://doi.org/10.1016/j.finel.2003.06.001
  2. Dynamic analysis of laminated cross-ply composite non-circular thick cylindrical shells using higher-order theory vol.39, pp.24, 2002, https://doi.org/10.1016/S0020-7683(02)00495-X
  3. Continuum damage modeling of composite laminated plates using higher order theory vol.99, 2013, https://doi.org/10.1016/j.compstruct.2012.11.038
  4. A unified formulation for vibration analysis of composite laminated shells of revolution including shear deformation and rotary inertia vol.98, 2013, https://doi.org/10.1016/j.compstruct.2012.11.001
  5. Investigation of supersonic flutter of thick doubly curved sandwich panels with CNT reinforced facesheets using higher-order structural theory vol.127, 2015, https://doi.org/10.1016/j.compstruct.2015.02.047
  6. A domain decomposition approach for vibration analysis of isotropic and composite cylindrical shells with arbitrary boundaries vol.95, 2013, https://doi.org/10.1016/j.compstruct.2012.06.022
  7. Higher-order Closed-form Solutions for Free Vibration of Laminated Composite and Sandwich Shells vol.8, pp.2, 2006, https://doi.org/10.1177/1099636206058779
  8. Thermal buckling of laminated cross-ply oval cylindrical shells vol.65, pp.2, 2004, https://doi.org/10.1016/j.compstruct.2003.10.018
  9. Buckling characteristics of cross-ply elliptical cylinders under axial compression vol.62, pp.1, 2003, https://doi.org/10.1016/S0263-8223(03)00079-5
  10. Free vibration analysis of functionally graded elliptical cylindrical shells using higher-order theory vol.69, pp.3, 2005, https://doi.org/10.1016/j.compstruct.2004.07.002
  11. Higher-order Closed-form Solutions for Free Vibration of Laminated Composite and Sandwich Shells vol.8, pp.3, 2006, https://doi.org/10.1177/1099636206062569
  12. Parametric instability of thick doubly curved CNT reinforced composite sandwich panels under in-plane periodic loads using higher-order shear deformation theory vol.24, pp.10, 2018, https://doi.org/10.1177/1077546316672973