Accurate prediction of critical conditions for shear-loaded panels
- 1 May 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (5) , 683-685
- https://doi.org/10.2514/3.7137
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Minimum-Weight Design of Stiffened Cylinders under Axial CompressionAIAA Journal, 1975
- General instability of eccentrically stiffened cylindrical panelsJournal of Aircraft, 1971