Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage

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Description

"The formulas given in this report provide a simplified method for the stress-analysis of fuselage bulkheads that are approximately circular rings of uniform cross section. Complicated load systems acting on a ring can usually be resolved into simplified load systems; and formulas for moment, axial force, and shear for such simplified load systems are given in this report. Illustrative examples showing the use of this method in practical stress-analysis work are also included" (p. 1).

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28 p. : ill.

Creation Information

Miller, Roy A. & Wood, Karl D. June 1933.

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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 2554 times, with 7 in the last month. More information about this report can be viewed below.

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  • Main Title: Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage
  • Series Title: NACA Technical Notes

Description

"The formulas given in this report provide a simplified method for the stress-analysis of fuselage bulkheads that are approximately circular rings of uniform cross section. Complicated load systems acting on a ring can usually be resolved into simplified load systems; and formulas for moment, axial force, and shear for such simplified load systems are given in this report. Illustrative examples showing the use of this method in practical stress-analysis work are also included" (p. 1).

Physical Description

28 p. : ill.

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  • Accession or Local Control No: 93R10618
  • OCLC: 1143006560
  • URL: http://digital.library.unt.edu/ark:/67531/metadc54214 External Link
  • Report No.: NACA-TN-462
  • Center for AeroSpace Information Number: 19930081328
  • Archival Resource Key: ark:/67531/metadc54214

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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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  • June 1933

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  • Nov. 14, 2011, 7:18 p.m.

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  • March 25, 2020, 12:11 p.m.

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Miller, Roy A. & Wood, Karl D. Formulas for the Stress Analysis of Circular Rings in a Monocoque Fuselage, report, June 1933; (https://digital.library.unt.edu/ark:/67531/metadc54214/: accessed April 24, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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