Buckling of Orthotropic, Curved, Sandwich Panels Subjected to Edge Shear Loads
- 1 July 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (7), 477-480
- https://doi.org/10.2514/3.59018
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Exact Solutions for Composite Laminates in Cylindrical BendingJournal of Composite Materials, 1969
- On the Nonlinear Oscillations of Plates Composed of Composite MaterialsJournal of Composite Materials, 1969
- The buckling behaviour in axial compression of slightly-curved panels, including the effect of shear deformabilityInternational Journal of Solids and Structures, 1968
- Fabrication and full-scale structural evaluation of glass-fabric reinforced plastic shells.Journal of Aircraft, 1968