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Validity of simplified analysis for the stability of laminated composite stiffened panels subjected to in-plane shear

  • Mallela, Upendra K. (Department of Civil Engineering, Indian Institute of Technology Roorkee) ;
  • Upadhyay, Akhil (Department of Civil Engineering, Indian Institute of Technology Roorkee)
  • Received : 2006.10.11
  • Accepted : 2007.02.27
  • Published : 2009.07.10

Abstract

Keywords

References

  1. Loughlan, J. (1994), "A finite strip analysis of the buckling characteristics of some composite stiffened shear panels", Compos. Struct., 27(3), 283-294 https://doi.org/10.1016/0263-8223(94)90089-2
  2. Mallela, U.K. and Upadhyay, A. (2006), "Buckling of laminated composite stiffened panels subjected to in-plane shear: A parametric study", Thin Wall. Struct., 44(3), 354-361 https://doi.org/10.1016/j.tws.2006.03.008
  3. Stroud, W.J., Greene, W.H. and Anderson, M.S. (1984), "Buckling loads of stiffened panels subjected to combined longitudinal compression and shear: Results obtained with PASCO, EAL, and STAGS computer programs", TP 2215, NASA
  4. Upadhyay, A. and Kalyanaraman, V. (2000), "Optimum design of fibre composite stiffened panels using genetic algorithms", Eng. Optimiz., 33, 201-220 https://doi.org/10.1080/03052150008940917

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