MINIMUM WEIGHT POTENTIALS FOR STIFFENED PLATES AND SHELLS
- 1 April 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (4) , 879-886
- https://doi.org/10.2514/3.1658
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The Optimum Design of Compression Surfaces having Unflanged Integral StiffenersJournal of the Royal Aeronautical Society, 1954
- The Design of Compression Structures for Minimum WeightJournal of the Royal Aeronautical Society, 1949
- Effects of Material Distribution on Strength of PanelsJournal of the Aeronautical Sciences, 1944