Elastic stability of thin-walled cylindrical and conical shells under axial compression
- 1 March 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (3) , 500-505
- https://doi.org/10.2514/3.2893
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- THE DEVELOPMENT OF DESIGN CRITERIA FOR ELASTIC STABILITY OF THIN SHELL STRUCTURESPublished by Defense Technical Information Center (DTIC) ,1960
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- Axisymmetrical Buckling of Circular Cones Under Axial CompressionJournal of Applied Mechanics, 1956
- Discussion: “Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial Compression” (Donnell, L. H., and Wan, C. C., 1950, ASME J. Appl. Mech., 17, pp. 73–83)Journal of Applied Mechanics, 1950
- Effect of Imperfections on Buckling of Thin Cylinders and Columns Under Axial CompressionJournal of Applied Mechanics, 1950
- The Buckling of Thin Cylindrical Shells Under Axial CompressionJournal of the Aeronautical Sciences, 1941
- Die Stabilität der KreiszylinderschaleArchive of Applied Mechanics, 1932
- The strength of tubular strutsProceedings of the Royal Society of London. Series A, Containing Papers of a Mathematical and Physical Character, 1928