Structural efficiency of orthotropic cylindrical shells subjected toaxial compression.
- 1 March 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (3), 481-485
- https://doi.org/10.2514/3.3461
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The Elastic Moduli of Fiber-Reinforced MaterialsJournal of Applied Mechanics, 1964
- MINIMUM WEIGHT POTENTIALS FOR STIFFENED PLATES AND SHELLSAIAA Journal, 1963
- Bending and Stretching of Certain Types of Heterogeneous Aeolotropic Elastic PlatesJournal of Applied Mechanics, 1961