Wind-tunnel tests of ailerons at various speeds 2: ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil

One of 257 reports in the series: NACA Advanced Confidential Reports available on this site.

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Description

Report presenting hinge-moment, lift, pressure difference across the balance, and pressure-distribution measurements in the two-dimensional test section of the stability tunnel on a 0.60 aileron-chord sealed internal-balance aileron on a specified NACA airfoil. The primary test objective was to determine the effect of speed on the action of the aileron.

Physical Description

[37] p. : ill.

Creation Information

Denaci, H. G. & Bird, J. D. June 1943.

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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 110 times , with 5 in the last month . More information about this report can be viewed below.

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  • Main Title: Wind-tunnel tests of ailerons at various speeds 2: ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil
  • Series Title: NACA Wartime Reports
  • Series Title: NACA Advanced Confidential Reports

Description

Report presenting hinge-moment, lift, pressure difference across the balance, and pressure-distribution measurements in the two-dimensional test section of the stability tunnel on a 0.60 aileron-chord sealed internal-balance aileron on a specified NACA airfoil. The primary test objective was to determine the effect of speed on the action of the aileron.

Physical Description

[37] p. : ill.

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  • Accession or Local Control No: 93R22220
  • URL: http://hdl.handle.net/2060/19930092930 External Link
  • Report No.: NACA-WR-L-432
  • Report No.: NACA-ACR-3F18
  • Center for AeroSpace Information Number: 19930092930
  • Archival Resource Key: ark:/67531/metadc61625

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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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Creation Date

  • June 1943

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • May 1, 2018, 9:21 a.m.

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Denaci, H. G. & Bird, J. D. Wind-tunnel tests of ailerons at various speeds 2: ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil, report, June 1943; (digital.library.unt.edu/ark:/67531/metadc61625/: accessed December 16, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.