Interlaminar Stresses in Laminated Cylindrical Shells of Composite Materials
- 1 September 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (9) , 1213-1218
- https://doi.org/10.2514/3.61455
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- On the Calculation of Interlaminar Normal Stress in Composite LaminateJournal of Composite Materials, 1974
- Free-Edge Delamination of Tensile CouponsJournal of Composite Materials, 1972
- Laminated Transversely Isotropic Cylindrical ShellsJournal of Applied Mechanics, 1971
- Moiré Analysis of the Interlaminar Shear Edge Effect in Laminated 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
- The natural vibrations of plates composed of composite materialsFibre Science and Technology, 1969
- A Simplified Method of Determining the Inplane Shear Stress-Strain Response of Unidirectional CompositesPublished by ASTM International ,1969
- Stresses in laminated composite cylinders.AIAA Journal, 1968
- Analysis of The Flexure Test of Bidirectional CompositesJournal of Composite Materials, 1967