Boundary layer effects in composite laminates
- 29 February 1980
- journal article
- Published by Elsevier in Fibre Science and Technology
- Vol. 13 (1), 49-71
- https://doi.org/10.1016/0015-0568(80)90028-7
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Approximate Three-Dimensional Solutions for Symmetric Laminates Under Inplane Loading *Journal of Composite Materials, 1971
- Finite-Element Analysis of Interlaminar Shear in Fibrous CompositesJournal 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
- A Simplified Method of Determining the Inplane Shear Stress-Strain Response of Unidirectional CompositesPublished by ASTM International ,1969