Some Effects of Wing Fences on the Lateral Stability Derivatives of a 60 Degree Delta Wing Oscillating Continuously in Yaw

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Description

Report presenting an investigation at low speed to determine some of the effects of wing fences on the lateral stability derivatives of a flat-plate 60 degree delta-wing model oscillating continuously in yaw. Results regarding the variation with angle of attack, effect of frequency, effect of amplitude, number of fences, and some effects of fence geometric characteristics are provided.

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29 p. : ill.

Creation Information

Riley, Donald R. July 11, 1956.

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

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  • Main Title: Some Effects of Wing Fences on the Lateral Stability Derivatives of a 60 Degree Delta Wing Oscillating Continuously in Yaw
  • Series Title: NACA Research Memorandums

Description

Report presenting an investigation at low speed to determine some of the effects of wing fences on the lateral stability derivatives of a flat-plate 60 degree delta-wing model oscillating continuously in yaw. Results regarding the variation with angle of attack, effect of frequency, effect of amplitude, number of fences, and some effects of fence geometric characteristics are provided.

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29 p. : ill.

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  • Accession or Local Control No: 93R18659
  • URL: http://hdl.handle.net/2060/19930089369 External Link
  • Report No.: NACA-RM-L56D13
  • Center for AeroSpace Information Number: 19930089369
  • Archival Resource Key: ark:/67531/metadc62717

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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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  • July 11, 1956

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • Jan. 17, 2019, 9:53 a.m.

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Riley, Donald R. Some Effects of Wing Fences on the Lateral Stability Derivatives of a 60 Degree Delta Wing Oscillating Continuously in Yaw, report, July 11, 1956; (https://digital.library.unt.edu/ark:/67531/metadc62717/: accessed April 19, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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