OPTIMUM DESIGN OF TRUSS-CORE SANDWICH CYLINDERS UNDER AXIAL COMPRESSION
- 1 July 1963
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 1 (7) , 1626-1630
- https://doi.org/10.2514/3.1868
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- The Optimum Design of Compression Surfaces having Unflanged Integral StiffenersJournal of the Royal Aeronautical Society, 1954