dc.contributor.author | A. J. Sobey | en_US |
dc.date.accessioned | 2014-10-21T15:56:08Z | |
dc.date.available | 2014-10-21T15:56:08Z | |
dc.date.issued | 1962 | en_US |
dc.identifier.other | ARC/R&M-3366 | en_US |
dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/3949 | |
dc.description.abstract | The theoretical estimation of the buckling strength of a cylinder loaded in axial compression is improved by the use of a more representative deflected form for the buckled cylinder than has previously been used. Kempner's buckling strength for dead-weight loading is reduced by 18%. The presentation of the magnitude and distribution of the constraint system required to maintain the mode is novel and instructive. | en_US |
dc.relation.ispartofseries | Aeronautical Research Council Reports & Memoranda | en_US |
dc.title | The buckling strength of a uniform circular cylinder loaded in axial compression | en_US |