Computation of Cantilever Airplane Wings

One of 1,438 items in the series: NACA Technical Memorandums available on this site.

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Description

The purpose of this treatise is, first of all, the determination of the effect of variously loaded spars on one another, since the neglect of this effect would present an economically very unfavorable computation method. The system of spars and cross-bars alone (whether solid or built-up) does not matter at first, the original assumption being that the spars are rigidly braced by the cross-bars.

Physical Description

[28] p. : ill.

Creation Information

Thalau, K. July 1925.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 66 times. More information about this report can be viewed below.

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Description

The purpose of this treatise is, first of all, the determination of the effect of variously loaded spars on one another, since the neglect of this effect would present an economically very unfavorable computation method. The system of spars and cross-bars alone (whether solid or built-up) does not matter at first, the original assumption being that the spars are rigidly braced by the cross-bars.

Physical Description

[28] p. : ill.

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  • Accession or Local Control No: 93R16412
  • URL: http://hdl.handle.net/2060/19930087122 External Link
  • Report No.: NACA-TM-325
  • Center for AeroSpace Information Number: 19930087122
  • Archival Resource Key: ark:/67531/metadc59245

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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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Creation Date

  • July 1925

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • Sept. 5, 2018, 12:27 p.m.

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Thalau, K. Computation of Cantilever Airplane Wings, report, July 1925; (https://digital.library.unt.edu/ark:/67531/metadc59245/: accessed March 28, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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