Buckling of stiffened multilayered circular cylindrical shells with different orthotropic moduli in tension and compression
- 1 May 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (5) , 917-923
- https://doi.org/10.2514/3.6296
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Buckling of circular cylindrical shells with different moduli in tension and compressionAIAA Journal, 1971
- Plastic buckling of eccentrically stiffened multilayered circular cylindrical shellsAIAA Journal, 1970
- Buckling of circular cylindrical shells with multiple orthotropic layers and eccentric stiffeners.AIAA Journal, 1968