Wind-tunnel investigation at transonic speeds of a jet control on a 35 degree swept wing: transonic-bump method

One of 5,164 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting an investigation in the high-speed tunnel using the transonic-bump method to determine the characteristics of a jet control consisting of numerous holes located at the 65-percent chord line of a 35 degree swept semispan wing with an NACA 65A006 airfoil section. Testing occurred over a range of Mach numbers, angles of attack, and ejection-pressure ratios. Results regarding rolling-moment coefficients and aerodynamic characteristics in pitch are provided.

Creation Information

Vogler, Raymond D. & Turner, Thomas R. February 8, 1956.

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  • Main Title: Wind-tunnel investigation at transonic speeds of a jet control on a 35 degree swept wing: transonic-bump method
  • Series Title: NACA Research Memorandums

Description

Report presenting an investigation in the high-speed tunnel using the transonic-bump method to determine the characteristics of a jet control consisting of numerous holes located at the 65-percent chord line of a 35 degree swept semispan wing with an NACA 65A006 airfoil section. Testing occurred over a range of Mach numbers, angles of attack, and ejection-pressure ratios. Results regarding rolling-moment coefficients and aerodynamic characteristics in pitch are provided.

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  • Accession or Local Control No: 93R18254
  • URL: http://hdl.handle.net/2060/19930088964 External Link
  • Report No.: NACA-RM-L55K09
  • Center for AeroSpace Information Number: 19930088964
  • Archival Resource Key: ark:/67531/metadc61814

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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

  • February 8, 1956

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

Description Last Updated

  • April 13, 2018, 2:21 p.m.

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Vogler, Raymond D. & Turner, Thomas R. Wind-tunnel investigation at transonic speeds of a jet control on a 35 degree swept wing: transonic-bump method, report, February 8, 1956; (digital.library.unt.edu/ark:/67531/metadc61814/: accessed September 23, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.