The analysis of buckling mode interaction of fiber-reinforced composite columns, modeled as plate assemblies, is presented. The main assumptions are linear elasticity; a linear fundamental equilibrium path; the existence of critical states that are coincident or near coincident; and a coupled path rising from a quadratic combination of modal displacements due to interaction. The formulation adopted is known as the W-formulation, in which the energy is written in terms of a sliding set of incremental coordinates, measured with respect to the fundamental path. The energy is then expressed with respect to a reduced modal coordinate basis, and the coupled solution arising from interaction is computed. An example of a pultruded composite I-column subjected to axial compression illustrates the procedure.
Skip Nav Destination
Article navigation
November 1995
Review Articles
Buckling Mode Interaction in Composite Plate Assemblies
Ioannis G. Raftoyiannis,
Ioannis G. Raftoyiannis
Department of Mechanical and Aerospace Engineering, W Virginia University, Morgantown WV 26506-6106 USA
Search for other works by this author on:
Luis A. Godoy,
Luis A. Godoy
Department of Civil Engineering, University of Puerto Rico, Mayaguez, Puerto Rico
Search for other works by this author on:
Ever J. Barbero
Ever J. Barbero
Department of Mechanical and Aerospace Engineering, W Virginia University, Morgantown WV 26506-6106 USA
Search for other works by this author on:
Ioannis G. Raftoyiannis
Department of Mechanical and Aerospace Engineering, W Virginia University, Morgantown WV 26506-6106 USA
Luis A. Godoy
Department of Civil Engineering, University of Puerto Rico, Mayaguez, Puerto Rico
Ever J. Barbero
Department of Mechanical and Aerospace Engineering, W Virginia University, Morgantown WV 26506-6106 USA
Appl. Mech. Rev. Nov 1995, 48(11S): S52-S60
Published Online: November 1, 1995
Article history
Online:
April 29, 2009
Citation
Raftoyiannis, I. G., Godoy, L. A., and Barbero, E. J. (November 1, 1995). "Buckling Mode Interaction in Composite Plate Assemblies." ASME. Appl. Mech. Rev. November 1995; 48(11S): S52–S60. https://doi.org/10.1115/1.3005083
Download citation file:
Get Email Alerts
Cited By
Related Articles
Modeling the Dynamic Response and Establishing Post-buckling/ Post Snap-thru Equilibrium of Discrete Structures via a Transient Analysis
J. Appl. Mech (September,1997)
Local Buckling and Failure of Pultruded Fiber-Reinforced Plastic Beams
J. Eng. Mater. Technol (April,1994)
Thermomechanical Buckling of Laminated Composite Plates Using Mixed, Higher-Order Analytical Formulation
J. Appl. Mech (November,2002)
End Effects in Prestrained Plates Under Compression
J. Appl. Mech (November,2004)
Related Proceedings Papers
Related Chapters
Mechanics of Instability-Related Delamination Growth
Composite Materials: Testing and Design (Ninth Volume)
Members in Compression
Design & Analysis of ASME Boiler and Pressure Vessel Components in the Creep Range
On the Exact Analysis of Non-Coherent Fault Trees: The ASTRA Package (PSAM-0285)
Proceedings of the Eighth International Conference on Probabilistic Safety Assessment & Management (PSAM)