Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees

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

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Description

Report presenting lift, drag, moment, and pressure-distribution measurements for the NACA 64A010, 64A410, 64A006, and 64A406 airfoil sections at high subsonic Mach numbers. Results regarding lift characteristics, drag characteristics, moment characteristics, pressure distributions, characteristics within the local supersonic regions, and characteristics above the stall are provided.

Physical Description

145 p. : ill.

Creation Information

Stivers, Louis S., Jr. March 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 2440 times , with 35 in the last month . More information about this report can be viewed below.

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  • Main Title: Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees
  • Series Title: NACA Technical Notes

Description

Report presenting lift, drag, moment, and pressure-distribution measurements for the NACA 64A010, 64A410, 64A006, and 64A406 airfoil sections at high subsonic Mach numbers. Results regarding lift characteristics, drag characteristics, moment characteristics, pressure distributions, characteristics within the local supersonic regions, and characteristics above the stall are provided.

Physical Description

145 p. : ill.

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Identifier

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  • Accession or Local Control No: 93R13174
  • URL: http://hdl.handle.net/2060/19930083884 External Link
  • Report No.: NACA-TN-3162
  • Center for AeroSpace Information Number: 19930083884
  • Archival Resource Key: ark:/67531/metadc57054

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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

  • March 1954

Added to The UNT Digital Library

  • Nov. 16, 2011, 7:33 a.m.

Description Last Updated

  • July 9, 2018, 11:29 a.m.

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Stivers, Louis S., Jr. Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees, report, March 1954; (digital.library.unt.edu/ark:/67531/metadc57054/: accessed December 16, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.