On the Mechanism of Buckling of a Circular Cylindrical Shell Under Axial Compression

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Description

The present paper deals with the buckling of a circular cylindrical shell under axial compression from the viewpoint of energy and the characteristics of deformation. It is shown first, both theoretically and experimentally, that the reason why the buckling of a cylindrical shell is quite different from that of a flat plate is attributable to the existence of a nearly developable surface far apart from the original cylindrical surface. Based upon this result, the experimental fact that the buckling is really not general but local, that is, that the buckled region is limited axially to a range of 1.5 times ... continued below

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46 p. : ill.

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Yoshimura, Yoshimaru July 1955.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 1994 times, with 27 in the last month. More information about this report can be viewed below.

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  • Main Title: On the Mechanism of Buckling of a Circular Cylindrical Shell Under Axial Compression
  • Series Title: NACA Technical Memorandums

Description

The present paper deals with the buckling of a circular cylindrical shell under axial compression from the viewpoint of energy and the characteristics of deformation. It is shown first, both theoretically and experimentally, that the reason why the buckling of a cylindrical shell is quite different from that of a flat plate is attributable to the existence of a nearly developable surface far apart from the original cylindrical surface. Based upon this result, the experimental fact that the buckling is really not general but local, that is, that the buckled region is limited axially to a range of 1.5 times the wave length of the lobe, is explained by the theoretical result that the minimum buckling load is smaller in the local buckling than in the general buckling case.

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46 p. : ill.

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  • Accession or Local Control No: 93R23165
  • URL: http://hdl.handle.net/2060/19930093840 External Link
  • Report No.: NACA-TM-1390
  • Center for AeroSpace Information Number: 19930093840
  • Archival Resource Key: ark:/67531/metadc62872

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National Advisory Committee for Aeronautics Collection

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915 to undertake, promote, and institutionalize aeronautical research. On October 1, 1958 the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA).

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  • July 1955

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  • Nov. 17, 2011, 5:13 p.m.

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  • Sept. 14, 2018, 12:37 p.m.

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Yoshimura, Yoshimaru. On the Mechanism of Buckling of a Circular Cylindrical Shell Under Axial Compression, report, July 1955; (https://digital.library.unt.edu/ark:/67531/metadc62872/: accessed February 26, 2020), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.