Creep Collapse of Long Cylindrical Shells Under High Temperature and External Pressure
- 1 March 1961
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 28 (3) , 177-188
- https://doi.org/10.2514/8.8922
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Propagation of Weak Disturbances in a Gas Subject to Relaxation EffectsJournal of the Aerospace Sciences, 1960
- A Study of Creep Collapse of a Long Circular Cylindrical Shell Under Uniform External PressureJournal of the Aerospace Sciences, 1959
- On Panel Flutter in the Presence of a Boundary LayerJournal of the Aerospace Sciences, 1959
- Elements of GasdynamicsPhysics Today, 1957
- Flutter of Rectangular Simply Supported Panels at High Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- Hydrodynamics of a Reacting and Relaxing FluidJournal of Applied Physics, 1957
- Piston Theory-A New Aerodynamic Tool for the AeroelasticianJournal of the Aeronautical Sciences, 1956
- Flexural vibrations of the walls of thin cylindrical shells having freely supported endsProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1949
- On Curved Shock WavesJournal of Mathematics and Physics, 1947
- LX. On the collapse of tubes by external pressure—IIIJournal of Computers in Education, 1915