Lift and Pitching Derivatives of Thin Sweptback Tapered Wings with Streamwise Tips and Subsonic Leading Edges at Supersonic Speeds

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Description

Note presenting the lift-due-to-pitching derivative and the damping-in-pitch derivative, which were derived for a series of thin sweptback tapered wings with streamwise tips and subsonic leading edges. The effects of camber and thickness were not considered.

Physical Description

46 p. : ill.

Creation Information

Malvestuto, Frank S., Jr. & Hoover, Dorothy M. February 1951.

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

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  • Main Title: Lift and Pitching Derivatives of Thin Sweptback Tapered Wings with Streamwise Tips and Subsonic Leading Edges at Supersonic Speeds
  • Series Title: NACA Technical Notes

Description

Note presenting the lift-due-to-pitching derivative and the damping-in-pitch derivative, which were derived for a series of thin sweptback tapered wings with streamwise tips and subsonic leading edges. The effects of camber and thickness were not considered.

Physical Description

46 p. : ill.

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  • Accession or Local Control No: 93R12243
  • URL: http://hdl.handle.net/2060/19930082953 External Link
  • Report No.: NACA-TN-2294
  • Center for AeroSpace Information Number: 19930082953
  • Archival Resource Key: ark:/67531/metadc55650

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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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  • February 1951

Added to The UNT Digital Library

  • Nov. 14, 2011, 10:26 p.m.

Description Last Updated

  • Nov. 26, 2018, 12:33 p.m.

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Malvestuto, Frank S., Jr. & Hoover, Dorothy M. Lift and Pitching Derivatives of Thin Sweptback Tapered Wings with Streamwise Tips and Subsonic Leading Edges at Supersonic Speeds, report, February 1951; (https://digital.library.unt.edu/ark:/67531/metadc55650/: accessed January 14, 2026), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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