Pressure-Distribution Measurements on the Tail Surfaces of a Rotating Model of the Design BFW - M31

One of 1,437 reports in the series: NACA Technical Memorandums available on this site.

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Description

In order to obtain insight into the flow conditions on tail surfaces on airplanes during spins, pressure-distribution measurements were performed on a rotating model of the design BFW-M31. For the time being, the tests were made for only one angle of attack (alpha = 60 degrees) and various angles of yaw and rudder angles. The results of these measurements are given; the construction of the model, and the test arrangement used are described. Measurements to be performed later and alterations planned in the test arrangement are pointed out.

Creation Information

Kohler, M. & Mautz, W. December 1949.

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

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  • Main Title: Pressure-Distribution Measurements on the Tail Surfaces of a Rotating Model of the Design BFW - M31
  • Series Title: NACA Technical Memorandums

Description

In order to obtain insight into the flow conditions on tail surfaces on airplanes during spins, pressure-distribution measurements were performed on a rotating model of the design BFW-M31. For the time being, the tests were made for only one angle of attack (alpha = 60 degrees) and various angles of yaw and rudder angles. The results of these measurements are given; the construction of the model, and the test arrangement used are described. Measurements to be performed later and alterations planned in the test arrangement are pointed out.

Source

  • ZWB Forschungsbericht Nr. 704; Rept-704

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  • URL: http://hdl.handle.net/2060/20050029436 External Link
  • Report No.: NACA-TM-1220
  • Center for AeroSpace Information Number: 20050029436
  • Archival Resource Key: ark:/67531/metadc64691

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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

  • December 1949

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • Jan. 11, 2018, 3:32 p.m.

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Kohler, M. & Mautz, W. Pressure-Distribution Measurements on the Tail Surfaces of a Rotating Model of the Design BFW - M31, report, December 1949; (digital.library.unt.edu/ark:/67531/metadc64691/: accessed October 21, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.