Effect of Chordwise Location of Maximum Thickness on the Supersonic Wave Drag of Sweptback Wings

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Description

Note presenting equations derived for the wave drag of sweptback untapered wings at zero lift with thin double-wedge sections and arbitrary chordwise location of maximum thickness. Calculations are presented for a representative supersonic plan form. Results regarding section wave drag, wing wave drag, comparison with two-dimensional theory, and comparison with tapered wings are provided.

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30 p. : ill.

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Margolis, Kenneth March 1948.

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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 168 times . More information about this report can be viewed below.

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  • Main Title: Effect of Chordwise Location of Maximum Thickness on the Supersonic Wave Drag of Sweptback Wings
  • Series Title: NACA Technical Notes

Description

Note presenting equations derived for the wave drag of sweptback untapered wings at zero lift with thin double-wedge sections and arbitrary chordwise location of maximum thickness. Calculations are presented for a representative supersonic plan form. Results regarding section wave drag, wing wave drag, comparison with two-dimensional theory, and comparison with tapered wings are provided.

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30 p. : ill.

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  • Accession or Local Control No: 93R11510
  • URL: http://hdl.handle.net/2060/19930082220 External Link
  • Report No.: NACA-TN-1543
  • Center for AeroSpace Information Number: 19930082220
  • Archival Resource Key: ark:/67531/metadc54538

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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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  • March 1948

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  • Nov. 14, 2011, 10:26 p.m.

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  • Aug. 23, 2018, 1:52 p.m.

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Margolis, Kenneth. Effect of Chordwise Location of Maximum Thickness on the Supersonic Wave Drag of Sweptback Wings, report, March 1948; (digital.library.unt.edu/ark:/67531/metadc54538/: accessed November 18, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.