Structural optimization of axially compressed, ring-stringer stiffened cylinders.
- 1 January 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (1) , 19-25
- https://doi.org/10.2514/3.28380
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Postbuckling behavior of orthotropic cylinders under axial compressionAIAA Journal, 1964
- Structural synthesis capability for integrally stiffened waffle platesAIAA Journal, 1963
- OPTIMUM DESIGN OF TRUSS-CORE SANDWICH CYLINDERS UNDER AXIAL COMPRESSIONAIAA Journal, 1963
- MINIMUM WEIGHT POTENTIALS FOR STIFFENED PLATES AND SHELLSAIAA Journal, 1963