Effect of nose shape and wing thickness ratio on the drag at zero lift of a missile having triangular wings and tails

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From Summary: "Free-flight tests have been made to determine the drag at zero lift of several configurations of a missile having triangular wings and tails. Base-pressure measurements were also obtained for some of the configurations. The results show that increasing the wing thickness ratio from 4 to 6 percent increased the wing drag by about 100 percent at M = 1.3 and by about 30 percent at M = 1.8."

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Hall, James R. & Sandahl, Carl A. May 31, 1950.

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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 619 times , with 18 in the last month . More information about this report can be viewed below.

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  • Main Title: Effect of nose shape and wing thickness ratio on the drag at zero lift of a missile having triangular wings and tails
  • Series Title: NACA Research Memorandums

Description

From Summary: "Free-flight tests have been made to determine the drag at zero lift of several configurations of a missile having triangular wings and tails. Base-pressure measurements were also obtained for some of the configurations. The results show that increasing the wing thickness ratio from 4 to 6 percent increased the wing drag by about 100 percent at M = 1.3 and by about 30 percent at M = 1.8."

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  • Accession or Local Control No: 68N83477
  • URL: http://hdl.handle.net/2060/19680068666 External Link
  • Report No.: NACA-RM-L50C16A
  • Center for AeroSpace Information Number: 19680068666
  • Archival Resource Key: ark:/67531/metadc53123

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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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  • May 31, 1950

Added to The UNT Digital Library

  • Nov. 11, 2011, 7:22 p.m.

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  • March 27, 2018, 1:58 p.m.

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Hall, James R. & Sandahl, Carl A. Effect of nose shape and wing thickness ratio on the drag at zero lift of a missile having triangular wings and tails, report, May 31, 1950; (digital.library.unt.edu/ark:/67531/metadc53123/: accessed July 21, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.