An analytical model of the behavior of an adhesive-bonded taper-taper composite joint under axial compressive loading has been developed using the Ritz Method. The model was based on laminated beam theory. A Fourier series was used to represent the transverse displacement variable and the Ritz method was used to derive an eigenvalue equation for adhesively bonded taper-taper composite joint. The smallest eigenvalue is the critical buckling load. Finite element analyses were performed on two unidirectional laminated beam joints with various taper angles to verify the analytical model. The effect of varying the taper angle, adhesive thickness and adhesive modulus on the critical buckling load were investigated analytically.
- Petroleum Institute
Buckling Analysis of a Taper-Taper Adhesive-Bonded Composite Joint
- Views Icon Views
- Share Icon Share
- Search Site
Helms, JE, Li, G, & Pang, S. "Buckling Analysis of a Taper-Taper Adhesive-Bonded Composite Joint." Proceedings of the ASME 2002 Engineering Technology Conference on Energy. Engineering Technology Conference on Energy, Parts A and B. Houston, Texas, USA. February 4–5, 2002. pp. 169-175. ASME. https://doi.org/10.1115/ETCE2002/CMDA-29072
Download citation file: