Interlaminar Stresses around Circular Cutouts in Composite Plates under Tension
- 1 November 1977
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (11), 1631-1637
- https://doi.org/10.2514/3.60828
Abstract
No abstract availableThis publication has 15 references indexed in Scilit:
- A Boundary Layer Theory - Part I: Laminated Composites in Plane StressJournal of Composite Materials, 1975
- Uniaxial Failure of Composite Laminates Containing Stress ConcentrationsPublished by ASTM International ,1975
- Interlaminar Stresses in Composite Laminates—An Approximate Elasticity SolutionJournal of Applied Mechanics, 1974
- Stress Fracture Criteria for Laminated Composites Containing Stress ConcentrationsJournal of Composite Materials, 1974
- On the Calculation of Interlaminar Normal Stress in Composite LaminateJournal of Composite Materials, 1974
- Tensile Strength of Notched CompositesJournal of Composite Materials, 1973
- Macroscopic Fracture Mechanics of Advanced Composite MaterialsJournal of Composite Materials, 1971
- 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
- Interlaminar Shear in Laminated Composites Under Generalized Plane StressJournal of Composite Materials, 1970