Critical shear loading of curved sandwich panels faced with fiber-reinforced plastic
Authors:
- 1 September 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 24 (9) , 1531-1536
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Shear Buckling of Stiff Core Anisotropic Sandwich PlateJournal of Engineering Mechanics, 1984
- Experimental Buckling Loads of Sandwich Panels with Carbon Fibre FaceplatesAeronautical Quarterly, 1973
- Buckling of Orthotropic, Curved, Sandwich Panels Subjected to Edge Shear LoadsJournal of Aircraft, 1972
- Buckling of Sandwich Panels with Laminated Face PlatesAeronautical Quarterly, 1972
- Critical Shear Loading of Curved Panels of Corrugated SheetsJournal of the Engineering Mechanics Division, 1970
- Finite deflection discrete element analysis of sandwich plates and cylindrical shells with laminated facesAIAA Journal, 1970
- Vibrations of orthotropic sandwich conical shells with free edgesInternational Journal of Mechanical Sciences, 1969
- Buckling of cylindrical and conical sandwich shells with orthotropicfacings.AIAA Journal, 1969
- Fabrication and full-scale structural evaluation of glass-fabric reinforced plastic shells.Journal of Aircraft, 1968
- Stability of circumferentially corrugated sandwich cylinders under combined loadsAIAA Journal, 1964