The Evaluation of Theoretical Critical Compression in Sandwich Plates
- 1 October 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (10) , 649-656
- https://doi.org/10.2514/8.2071
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Bifurcation Criterion and Plastic Buckling of Plates and ColumnsJournal of the Aeronautical Sciences, 1950
- Column Behavior in the Plastic Stress RangeJournal of the Aeronautical Sciences, 1950
- Column Curves for Magnesium-Alloy SheetJournal of the Aeronautical Sciences, 1949
- Bending and Buckling of Sandwich BeamsJournal of the Aeronautical Sciences, 1948
- Cylindrical Buckling of Sandwich PlatesJournal of Applied Mechanics, 1946
- The Buckling of Sandwich-Type PanelsJournal of the Aeronautical Sciences, 1945
- The Stabilisation of a Thin Sheet by a Continuous Supporting MediumJournal of the Royal Aeronautical Society, 1940