INFLUENCE OF IMPERFECTIONS AND EDGE RESTRAINT ON THE BUCKLING OF AXIALLY COMPRESSED CYLINDERS
- 18 April 1966
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Low Buckling Stresses of Axially Compressed Circular Cylindrical Shells of Finite LengthJournal of Applied Mechanics, 1965