A three-dimensional analysis of edge effects in composite laminates with circular holes
- 31 December 1990
- journal article
- Published by Elsevier in Composite Structures
- Vol. 15 (2), 115-136
- https://doi.org/10.1016/0263-8223(90)90002-v
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- An Efficient Method for the Calculation of Interlaminar Stresses in Composite MaterialsJournal of Applied Mechanics, 1986
- On the Prediction of the Initiation of Delamination in a [0/90]S Laminate with a Circular HoleJournal of Composite Materials, 1984
- The Effect of Geometry on Interlaminar Stresses of [0/90]s Composite Laminates with Circular HolesJournal of Composite Materials, 1984
- Superposition Method for Analysis of Free-Edge StressesJournal of Composite Materials, 1983
- Interlaminar Stresses at a Hole in a Composite Member Subjected to In-Plane LoadingJournal of Composite Materials, 1983
- Effect of Stacking Sequence and Lay-Up Angle on Free Edge Stresses Around a Hole in a Laminated Plate Under TensionJournal of Composite Materials, 1978
- Edge Effects in Angle-Ply Composite Laminates*Journal of Composite Materials, 1977
- Some New Results on Edge Effect in Symmetric Composite LaminatesJournal of Composite Materials, 1977
- Some observations on the interlaminar strength of composite laminatesInternational Journal of Mechanical Sciences, 1973
- The Influence of Stacking Sequence on Laminate StrengthJournal of Composite Materials, 1971