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Free And Forced Vibrations of a Post-Buckled Delaminated Beam-Plate Resting on a Two Parameter Elastic Foundation

Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
In this study, the free and forced vibrations of a delaminated beam-plate resting on a two-parameter (Pasternak type) elastic foundation are investigated. We consider a homogeneous isotropic clamped beam-plate compressed axially and subject to an external time dependent force. In order to study the vibration of the delaminated beam-plate relative to a post-buckled state we should solve the static deformations. This has been accomplished by the successive substitution method.The free and forced vibration analysis are then performed. Results are represented in both graphical and tabulated forms and shows that the natural frequencies are affected by the change in the delamination length, depth and location and also affected by the change in the elastic foundation parameters.
Rocznik
Strony
207--222
Opis fizyczny
Bibliogr. 14 poz.
Twórcy
autor
  • Faculty of Engineering, Cairo University Giza, Egypt
  • Faculty of Engineering, Cairo University Giza, Egypt
autor
  • Faculty of Engineering, Cairo University Giza, Egypt
Bibliografia
  • [1] Chai, H, Babcock, CD and Knauss, B: One Dimensional Modeling of Failure of Laminated Plates by Delamination Buckling, International Journal of Solids and Structures, (1981), 17, 1069-1083.
  • [2] Wang, JTS, Liu, YY and Gibb, Y: Vibration of Split Beams, Journal of Sound and Vibration, (1982), 84, 491-502.
  • [3] Simitses, GJ, Sallam, SN and Yin, WL: Effect of Delamination of Axially Loaded Homogeneous Laminated Plates, AIAA, (1985), 23, 1437-1444.
  • [4] Yin, WL, Sallam, SN and Simitses, GJ: Ultimate Axial Load Capacity of a Delaminated Beam Plate, AIAA, (1986), 24(1), 123-128.
  • [5] Kardomateas, GA and Schmueser, DW: Buckling and Postbuckling of Delaminated Composites Under Compressive Loads Including Transverse Shear Effect, AIAA, (1988), 26, 337-334.
  • [6] Lee-Chubg, S: Flutter of Composite Laminated Beam-Plates with Delamination, AIAA, (1992), 30(10), 2504-2511.
  • [7] Jane, KC and Chen, JC: Postbuckling Deformation and Vibration of a delaminated Beam Plate with Arbitrary Delamination Location, Mechanics Research Communications, (1998), 25(3), 337-351.
  • [8] Chang, TP and Liang, JY: Vibration of Postbuckled Delaminated Beam-Plates, International Journal of Solids Structures, (1998), 35(12), 1199-1217.
  • [9] Hui-Shen, S: Large Deflection of Composite Laminated Plates Under Transverse and Inplane Loads and Resting on Elastic Foundation, Composite Structures, (1999), 45, 115-123.
  • [10] Patel, BP, Ganapathi, M, and Touratier, M: Non-Linear Free Flexural Vibrations / Postbuckling Analysis of Laminated Orthotropic Beams / Columns on a Two Parameter Elastic Foundation, Composite Structures, (1999), 46, 189-196.
  • [11] Brandinelli, L and Massabo, R: Free Vibrations of Through Thickness Reinforced Delaminated Beams, 15 th ASCE Engineering Mechanics Conference June 2-5, 2002, Columbia University, New York.
  • [12] Clough, RW and Penzien, J: Dynamics of Structures, McGraw-Hill Book Company.
  • [13] Timoshenko, S and Woinowsky-Krieger, S: Theory of Plates and Shells, (1940), McGraw-Hill Book Company.
  • [14] Timoshenko, S and Gere, JM: Theory of Elastic Stability, (1961), McGraw-Hill Book Company.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-LOD5-0006-0027
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