Stress and buckling of nonuniformly heated cylindrical and conical shells.
- 1 December 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (12) , 2314-2321
- https://doi.org/10.2514/3.6515
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Analysis of ring-stiffened shells of revolution under combined thermal and mechanical loadingAIAA Journal, 1971
- Stress, buckling and vibration of prismatic shellsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Design criteria for axially loaded cylindrical shellsJournal of Spacecraft and Rockets, 1970
- Nonlinear thermal elastic buckling of conical shellsNuclear Engineering and Design, 1968
- Computer analysis of asymmetric buckling of ring-stiffened orthotropic shells of revolution.AIAA Journal, 1968
- Thermal buckling of conical shells.AIAA Journal, 1967
- The buckling behavior of uniformly heated thin circular cylindrical shellsExperimental Mechanics, 1966
- Buckling of thin cylindrical shells heated along an axial stripExperimental Mechanics, 1965
- Analysis of Shells of Revolution Subjected to Symmetrical and Nonsymmetrical LoadsJournal of Applied Mechanics, 1964
- Buckling at High TemperatureJournal of the Royal Aeronautical Society, 1957