Buckling Under External Pressure of Cylindrical Shells Evenly Stiffened by Rings Only
- 1 June 1957
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 24 (6), 437-447
- https://doi.org/10.2514/8.3874
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Similarity Solution for a Spherical Shock WaveJournal of Applied Physics, 1955
- Buckling Stress of Thin Cylindrical Clamped Shells Subject to Hydrostatic PressureJournal of the Aeronautical Sciences, 1954
- Three-Dimensional Laminar Boundary-Layer FlowJournal of the Aeronautical Sciences, 1953
- TESTS OF THE ELASTIC STABILITY OF A RING-STIFFENED CYLINDRICAL SHELL, MODEL BR-5 (LAMBDA= 1.705), SUBJECTED TO HYDROSTATIC PRESSUREPublished by Defense Technical Information Center (DTIC) ,1953
- Lift on Inclined Bodies of Revolution in Hypersonic FlowJournal of the Aeronautical Sciences, 1950
- Theory and Tests on the Plastic Stability of Plates and ShellsJournal of the Aeronautical Sciences, 1949