Journal of the Korean Society for Advanced Composite Structures (복합신소재구조학회 논문집)

Korean Society for Advanced Composite Structures (한국복합신소재구조학회)
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Use of Buckling Coefficient in Predicting Buckling Load of Plates with and without Holes

홀의 유무에 따른 평판 좌굴하중 산정을 위한 좌굴계수

  • Behzad, Mohamazadeh (Department of Civil and Environmental Engineering, Sejong University) ;
  • Noh, Hyuk-Chun (Department of Civil and Environmental Engineering, Sejong University)
  • Received : 2014.09.12
  • Accepted : 2014.09.23
  • Published : 2014.09.30
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Abstract

Buckling, a form of failure happened to plated structures, is investigated in this study. The main focus is to investigate the effects of thickness of the plates having through-thickness holes on buckling when the plate is subjected to in-plane compression. Plates having length of 200mm and width of 100mm are chosen to have thickness in range from 0.50mm to 10mm. Two holes of diameters of 20mm are implemented in plates. The finite element procedure using ABAQUS is applied for analyses. Then using the Gerard and Becker equation compressive buckling coefficients, Kc, are calculated and presented to enable engineers to calculate buckling load for the desired plate with holes in specific dimension. In order to generalize the obtained results, verification analysis has been performed by taking plates having different dimensions from the original ones used in this study. The verification showed the capability of buckling coefficients to predict buckling stresses of plates in various dimensions.

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References

  1. Chio et al. (2012), "An Analytical Study on the Buckling of Orthotropic Plates and Local Buckling of Compression Members", Journal of Korean Society for Advanced Composite Structures, Vol. 3, No. 1, pp. 21-28. https://doi.org/10.11004/kosacs.2012.3.1.021
  2. Cristopher D. M, B.W. Schafer (2009), Elastic buckling of thin plates with holes in compression or bending, journal of Thin-Walled Structures, Vol.47, pp. 1597-1607. https://doi.org/10.1016/j.tws.2009.05.001
  3. G. M. Hong, C. M. Wang and T. J. Tan (1993), Analytical buckling solutions for circular Mindlin plates: inclusion of in-plane pre-buckling deformation, Archive of Applied Mechanics, Vol. 63, 534-542. https://doi.org/10.1007/BF00804755
  4. Gerard, G. and Becker, H(1957), Handbook of structural stability- Buckling of flat plates, National advisory committee for aeronautics, New York university.
  5. Husam Al Qablan, Hasan Katkhuda and Hazim Dwairi (2009), Assessment of the Buckling Behavior of Square Composite Plates with Circular Cutout Subjected to In-Plane Shear, Jordan Journal of Civil Engineering, Vol. 3, No. 2.
  6. Jodoin, et al (2012), Analysis of Buckling, Vol. III
  7. Khaled M., El-Sawy, Aly S. Nazmy (2001), Effect of aspect ratio on the elastic buckling of uniaxially loaded plates with eccentric holes, Thin-Walled Structures, Vol. 39, pp. 983-998. https://doi.org/10.1016/S0263-8231(01)00040-4
  8. Kwon and Jung (2012), "Comparison of Improved Explicit Method and Predictor Correct $\alpha$-Method", Journal of Korean Society for Advanced Composite Structures, Vol. 3, No. 4, pp. 1-9. https://doi.org/10.11004/kosacs.2012.3.4.001
  9. Mitao Ohga, Tsunemi Shigematsu, & Kouichi Kawaguchi (1995), "Buckling Analysis of Thin-Walled Members With Variable Thickness", Journal of Structural Engineering, Vol. 121:919-924. https://doi.org/10.1061/(ASCE)0733-9445(1995)121:6(919)
  10. Tom, Pollock (1993), Introduction to Buckling, Dept. of Aerospace Engineering, Texaz A&M University, USA.
  11. William L., (1998), Mechanical and Thermal Buckling Behavior of Rectangular Plates With Different Central Cutouts, Dryden Flight Research Center, NASA, US.

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