Edge restraint effect on buckling of compressed curved panels.
- 1 January 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (1), 187-189
- https://doi.org/10.2514/3.4476
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- INFLUENCE OF IMPERFECTIONS AND EDGE RESTRAINT ON THE BUCKLING OF AXIALLY COMPRESSED CYLINDERSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- The effect of the edge conditions on the buckling of thin-walled circular cylindrical shells in axial compressionPublished by Springer Nature ,1966
- Some perturbation solutions in laminar boundary-layer theoryJournal of Fluid Mechanics, 1963