Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01

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Robinson, Ross B July 9, 1958.

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

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  • Main Title: Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01
  • Series Title: NACA Research Memorandums

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  • Accession or Local Control No: 93R19359
  • URL: http://hdl.handle.net/2060/19930090069 External Link
  • Report No.: NACA-RM-L58C18
  • Center for AeroSpace Information Number: 19930090069
  • Archival Resource Key: ark:/67531/metadc64112

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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 9, 1958

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • April 9, 2018, 5:31 p.m.

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Thumbnail image of item number 1 in: 'Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01'.
Thumbnail image of item number 2 in: 'Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01'.
Thumbnail image of item number 3 in: 'Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01'.
Thumbnail image of item number 4 in: 'Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01'.

PDF Version Also Available for Download.

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Robinson, Ross B. Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01, report, July 9, 1958; (digital.library.unt.edu/ark:/67531/metadc64112/: accessed April 25, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.