A Boundary Layer Theory - Part II: Extension of Laminated Finite Strip
- 1 January 1975
- journal article
- research article
- Published by SAGE Publications in Journal of Composite Materials
- Vol. 9 (1), 42-52
- https://doi.org/10.1177/002199837500900105
Abstract
Using a newly developed boundary layer theory for laminated compos ites, a complete analytical solution is obtained for all the interlaminar shear stresses as well as the normal or "peel" stress of a finite strip in unidirec tional extension. Results obtained by the present analysis are compared to the finite-difference solution of Pipes and Pagano, and to the analytical solution of Puppo and Evensen.Keywords
This publication has 5 references indexed in Scilit:
- A Boundary Layer Theory - Part I: Laminated Composites in Plane StressJournal of Composite Materials, 1975
- Approximate Three-Dimensional Solutions for Symmetric Laminates Under Inplane Loading *Journal of Composite Materials, 1971
- The Influence of Stacking Sequence on Laminate StrengthJournal of Composite Materials, 1971
- Interlaminar Stresses in Composite Laminates Under Uniform Axial ExtensionJournal of Composite Materials, 1970
- Interlaminar Shear in Laminated Composites Under Generalized Plane StressJournal of Composite Materials, 1970