The inward bulge type buckling of monocoque cylinders 2: experimental investigation of the buckling in combined bending and compression

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This paper is the second part of a series of reports on the inward bulge type buckling of monocoque cylinders. It presents the results of an experimental investigation of buckling in combined bending and compression. In the investigation it was found that the theory developed in part I of the present series predicts the buckling load in combined bending and compression with the same degree of accuracy as the older theory does in pure bending. In the realm covered by the experiments no systematic variation of the parameter N was observed. The analysis of the test results afforded a check ... continued below

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Hoff, N. J.; Fuchs, S. J. & Cirillo, Adam J. October 1944.

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  • Main Title: The inward bulge type buckling of monocoque cylinders 2: experimental investigation of the buckling in combined bending and compression
  • Series Title: NACA Technical Notes

Description

This paper is the second part of a series of reports on the inward bulge type buckling of monocoque cylinders. It presents the results of an experimental investigation of buckling in combined bending and compression. In the investigation it was found that the theory developed in part I of the present series predicts the buckling load in combined bending and compression with the same degree of accuracy as the older theory does in pure bending. In the realm covered by the experiments no systematic variation of the parameter N was observed. The analysis of the test results afforded a check on the theories of buckling of a curved panel. The agreement between experiment and theory was reasonably good. In addition, the effect of the end conditions upon the stress distribution under loads and upon initial stresses was investigated.

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"II."

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  • Accession or Local Control No: 93R14295
  • URL: http://hdl.handle.net/2060/19930085005 External Link
  • Report No.: NACA-TN-939
  • Center for AeroSpace Information Number: 19930085005
  • Archival Resource Key: ark:/67531/metadc56874

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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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  • October 1944

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • June 26, 2018, 4:12 p.m.

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Hoff, N. J.; Fuchs, S. J. & Cirillo, Adam J. The inward bulge type buckling of monocoque cylinders 2: experimental investigation of the buckling in combined bending and compression, report, October 1944; (digital.library.unt.edu/ark:/67531/metadc56874/: accessed October 20, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.