Structural Engineering and Mechanics

  • 제3권3호
  • /
  • Pages.229-244
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  • 1995
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  • 1225-4568(pISSN)
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  • 1598-6217(eISSN)
테크노프레스 (Techno-Press)
권호 표지
DOI QR코드

DOI QR Code

Effects of damping on the parametric instability behaviour of plates under localized edge loading (compression or tension)

  • Deolasi, P.J. (Department of Aerospace Engineering, Indian Institute of Technology) ;
  • Datta, P.K. (Department of Aerospace Engineering, Indian Institute of Technology)
  • 발행 : 1995.05.25
⟨ 이전 논문 다음 논문 ⟩

초록

The parametric instability behaviour of a plate subjected to localized in-plane compressive or tensile periodic edge loading is studied, considering the effects of damping into the system. Different edge loading cases have been considered. Damping has been introduced in the form of proportional damping. Dynamic instability behaviour under compressive or tensile periodic edge loading shows that the instability regions are influenced by the load band width and its location on the edge. The effects of damping on the instability regions show that there is a critical value of dynamic load factor beyond which the plate becomes dynamically unstable. The critical dynamic load factor increases as damping increases. Damping generally reduces the widths of the instability regions.

키워드

참고문헌

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피인용 문헌

  1. Combination Resonance Instability of Curved Panels with Cutout Subjected to Nonuniform Loading with Damping vol.134, pp.7, 2008, https://doi.org/10.1061/(ASCE)0733-9399(2008)134:7(555)
  2. Research Advances in the Dynamic Stability Behavior of Plates and Shells: 1987–2005—Part I: Conservative Systems vol.60, pp.2, 2007, https://doi.org/10.1115/1.2515580
  3. Dynamic Stability of Superelliptical Plates Resting on Elastic Foundations under Periodic In-Plane Loads vol.140, pp.1, 2014, https://doi.org/10.1061/(ASCE)EM.1943-7889.0000630
  4. Parametric combination resonance instability characteristics of laminated composite curved panels with circular cutout subjected to non-uniform loading with damping vol.49, pp.3, 2007, https://doi.org/10.1016/j.ijmecsci.2006.09.001
  5. Research Advances on Tension Buckling Behaviour of Aerospace Structures: A Review vol.12, pp.1, 2011, https://doi.org/10.5139/ijass.2011.12.1.1