Structural optimization of axially compressed cylinders, consideringring-stringer eccentricity effects.
- 1 August 1966
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 3 (8) , 1263-1268
- https://doi.org/10.2514/3.28637
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Structural optimization of axially compressed cylinders, consideringring-stringer eccentricity effects.Journal of Spacecraft and Rockets, 1966
- Structural optimization of axially compressed, ring-stringer stiffened cylinders.Journal of Spacecraft and Rockets, 1966
- Stability of stiffened cylinders.AIAA Journal, 1965
- FURTHER REMARKS ON THE EFFECT OF ECCENTRICITY OF STIFFENERS ON THE GENERAL INSTABILITY OF STIFFENED CYLINDRICAL SHELLSPublished by Defense Technical Information Center (DTIC) ,1965
- Effects of asymmetric stiffening on buckling of shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Static and dynamic effects on eccentric stiffening of plates and cylindrical shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965
- Effect of Eccentricity of Stiffeners on the General Instability of Stiffened Cylindrical Shells under Hydrostatic PressureJournal of Mechanical Engineering Science, 1963