Comparative Flight and Full-Scale Wind-Tunnel Measurements of the Maximum Lift of an Airplane

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Description

"Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-scale wind tunnel and in flight. The results from the two types of test were in satisfactory agreement. It was found that, when the airplane was rotated positively in pitch through the angle of stall at rates of the order of 0.1 degree per second, the maximum lift coefficient was considerably higher than that obtained in the standard tests, in which the forces are measured with the angles of attack fixed. Scale effect on the maximum lift coefficient was also investigated" (p. 161).

Physical Description

161 - 167 p. : ill.

Creation Information

Silverstein, Abe; Katzoff, S. & Hootman, James A. October 26, 1937.

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

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  • Main Title: Comparative Flight and Full-Scale Wind-Tunnel Measurements of the Maximum Lift of an Airplane
  • Series Title: NACA Technical Reports

Description

"Determinations of the power-off maximum lift of a Fairchild 22 airplane were made in the NACA full-scale wind tunnel and in flight. The results from the two types of test were in satisfactory agreement. It was found that, when the airplane was rotated positively in pitch through the angle of stall at rates of the order of 0.1 degree per second, the maximum lift coefficient was considerably higher than that obtained in the standard tests, in which the forces are measured with the angles of attack fixed. Scale effect on the maximum lift coefficient was also investigated" (p. 161).

Physical Description

161 - 167 p. : ill.

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  • Accession or Local Control No: 93R20983
  • URL: http://hdl.handle.net/2060/19930091693 External Link
  • Report No.: NACA-TR-618
  • Center for AeroSpace Information Number: 19930091693
  • Archival Resource Key: ark:/67531/metadc66276

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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

  • October 26, 1937

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • July 23, 2018, 3:59 p.m.

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Silverstein, Abe; Katzoff, S. & Hootman, James A. Comparative Flight and Full-Scale Wind-Tunnel Measurements of the Maximum Lift of an Airplane, report, October 26, 1937; (digital.library.unt.edu/ark:/67531/metadc66276/: accessed November 13, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.