Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips: Subsonic leading edges and supersonic trailing edges

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Description

Report presenting the theoretical spanwise distributions of circulation resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration calculated for a series of thin, sweptback, tapered wings with streamwise tips.

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221 p. : ill.

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Hannah, Margery E. & Margolis, Kenneth December 1952.

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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 Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 58 times . More information about this report can be viewed below.

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  • Main Title: Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips: Subsonic leading edges and supersonic trailing edges
  • Series Title: NACA Technical Notes

Description

Report presenting the theoretical spanwise distributions of circulation resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration calculated for a series of thin, sweptback, tapered wings with streamwise tips.

Physical Description

221 p. : ill.

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  • Accession or Local Control No: 93R12797
  • URL: http://hdl.handle.net/2060/19930083507 External Link
  • Report No.: NACA-TN-2831
  • Center for AeroSpace Information Number: 19930083507
  • Archival Resource Key: ark:/67531/metadc56388

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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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  • December 1952

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

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  • April 5, 2018, 5 p.m.

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Thumbnail image of item number 1 in: 'Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips: Subsonic leading edges and supersonic trailing edges'.
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Hannah, Margery E. & Margolis, Kenneth. Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips: Subsonic leading edges and supersonic trailing edges, report, December 1952; (digital.library.unt.edu/ark:/67531/metadc56388/: accessed February 21, 2019), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.