A Unified Theory for Creep Buckling Under Normal Loads
- 1 June 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (6) , 658-661
- https://doi.org/10.2514/8.9578
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Creep Collapse of Long Cylindrical Shells Under High Temperature and External PressureJournal of the Aerospace Sciences, 1961
- Creep BucklingAeronautical Quarterly, 1956
- On the Nonexistence of a Finite Critical Time for Linear Viscoelastic ColumnsJournal of the Aeronautical Sciences, 1953
- Creep Buckling of ColumnsJournal of the Aeronautical Sciences, 1952
- Creep Deflections in ColumnsJournal of Applied Physics, 1947
- Viscosity, Plasticity, and Diffusion as Examples of Absolute Reaction RatesThe Journal of Chemical Physics, 1936