Section characteristics of an NACA 0006 airfoil with area suction near the leading edge

One of 4,119 reports in the series: NACA Technical Notes available on this site.

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Description

Report presenting an investigation of the low-speed two-dimensional aerodynamic characteristics of an NACA 0006 airfoil with area suction near the leading edge. For a given increase in lift coefficient, the minimum suction quantity required was related to the magnitude of the difference between the external pressure coefficients at the leading and trailing edges of the porous area. Results regarding the stall of the model, effect of chordwise extent of suction, chordwise variation of suction velocity, typical aerodynamic characteristics, effect of free-stream velocity, effect of a deflected flap, and some design considerations are provided.

Physical Description

47 p. : ill.

Creation Information

Weiberg, James A. & Dannenberg, Robert E. September 1954.

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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 1810 times , with 20 in the last month . More information about this report can be viewed below.

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  • Main Title: Section characteristics of an NACA 0006 airfoil with area suction near the leading edge
  • Series Title: NACA Technical Notes

Description

Report presenting an investigation of the low-speed two-dimensional aerodynamic characteristics of an NACA 0006 airfoil with area suction near the leading edge. For a given increase in lift coefficient, the minimum suction quantity required was related to the magnitude of the difference between the external pressure coefficients at the leading and trailing edges of the porous area. Results regarding the stall of the model, effect of chordwise extent of suction, chordwise variation of suction velocity, typical aerodynamic characteristics, effect of free-stream velocity, effect of a deflected flap, and some design considerations are provided.

Physical Description

47 p. : ill.

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  • Accession or Local Control No: 93R13259
  • URL: http://hdl.handle.net/2060/19930083969 External Link
  • Report No.: NACA-TN-3285
  • Center for AeroSpace Information Number: 19930083969
  • Archival Resource Key: ark:/67531/metadc57184

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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).

Technical Report Archive and Image Library

This selection of materials from the Technical Report Archive and Image Library (TRAIL) includes hard-to-find reports published by various government agencies. The technical publications contain reports, images, and technical descriptions of research performed for U.S. government agencies. Topics range from mining, desalination, and radiation to broader physics, biology, and chemistry studies. Some reports include maps, foldouts, blueprints, and other oversize materials.

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Creation Date

  • September 1954

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

Description Last Updated

  • June 11, 2018, 12:26 p.m.

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Weiberg, James A. & Dannenberg, Robert E. Section characteristics of an NACA 0006 airfoil with area suction near the leading edge, report, September 1954; (digital.library.unt.edu/ark:/67531/metadc57184/: accessed December 14, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.