Optimum stiffened cylinders for combined axial compression and internal or external pressure.
- 1 June 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (6) , 690-699
- https://doi.org/10.2514/3.29332
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Inversion of the Eccentricity Effect in Stiffened Cylindrical Shells Buckling under External PressureJournal of Mechanical Engineering Science, 1966
- Structural optimization of axially compressed cylinders, consideringring-stringer eccentricity effects.Journal of Spacecraft and Rockets, 1966
- Combined loads minimum weight analysis of stiffened plates and shells.Journal of Spacecraft and Rockets, 1966
- Structural optimization of axially compressed, ring-stringer stiffened cylinders.Journal of Spacecraft and Rockets, 1966
- Axial buckling of pressurized imperfect cylindrical shellsAIAA Journal, 1965
- Elastic stability of thin-walled cylindrical and conical shells under combined internal pressure and axial compressionAIAA Journal, 1965
- Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells under Hydrostatic PressureJournal of Mechanical Engineering Science, 1963
- The Stability of Thin-Walled Unstiffened Circular Cylinders Under Axial Compression Including the Effects of Internal PressureJournal of the Aeronautical Sciences, 1957