Design criteria for axially loaded cylindrical shells
- 1 June 1970
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 7 (6), 714-720
- https://doi.org/10.2514/3.30025
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Imperfection sensitivity of stringer stiffened cylinders.AIAA Journal, 1968
- Influence of stiffener eccentricity and end moment on stability of cylinders in compression.AIAA Journal, 1966
- Postbuckling equilibrium of axially compressed circular cylindrical shells.AIAA Journal, 1966
- Structural optimization of axially compressed, ring-stringer stiffened cylinders.Journal of Spacecraft and Rockets, 1966
- EXPERIMENTS ON AXIAL COMPRESSIVE GENERAL INSTABILITY OF MONOLITHIC RING-STIFFENED CYLINDERSAIAA Journal, 1963
- The Stability Under Axial Compression and Lateral Pressure of Circular-Cylindrical Shells With a Soft Elastic CoreJournal of the Aerospace Sciences, 1962
- BUCKLING OF CYLINDERS OF SANDWICH CONSTRUCTION IN AXIAL COMPRESSIONPublished by Defense Technical Information Center (DTIC) ,1957
- The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal PressureJournal of the Aeronautical Sciences, 1957
- Simplified Analysis of General Instability of Stiffened Shells in Pure BendingJournal of the Aeronautical Sciences, 1949
- The Buckling of Thin Cylindrical Shells Under Axial CompressionJournal of the Aeronautical Sciences, 1941