An experimental study of five annular air inlet configurations at subsonic and transonic speeds

One of 5,157 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting an investigation of an NACA 1-80-100 nose inlet fitted alternately with an elliptical, a parabolic, a 14 degree-inch conical, and a 22 degree-inch conical central body at subsonic and transonic speeds in the 8-foot transonic tunnel. Drag, surface-pressure, and pressure-recovery measurements were obtained at 0 degrees angle of attack through a range of Mach numbers. Results regarding tunnel boundary interference, surface-pressure distribution, external drag, pressure recovery, and propulsive thrust comparison are provided.

Physical Description

86 p. : ill.

Creation Information

Pendley, Robert E.; Milillo, Joseph R.; Fleming, Frank F. & Bryan, Carroll R. August 19, 1953.

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This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided by the UNT Libraries Government Documents Department to the UNT Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 86 times. More information about this report can be viewed below.

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  • Main Title: An experimental study of five annular air inlet configurations at subsonic and transonic speeds
  • Series Title: NACA Research Memorandums

Description

Report presenting an investigation of an NACA 1-80-100 nose inlet fitted alternately with an elliptical, a parabolic, a 14 degree-inch conical, and a 22 degree-inch conical central body at subsonic and transonic speeds in the 8-foot transonic tunnel. Drag, surface-pressure, and pressure-recovery measurements were obtained at 0 degrees angle of attack through a range of Mach numbers. Results regarding tunnel boundary interference, surface-pressure distribution, external drag, pressure recovery, and propulsive thrust comparison are provided.

Physical Description

86 p. : ill.

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  • Accession or Local Control No: 93R18420
  • URL: http://hdl.handle.net/2060/19930089130 External Link
  • Report No.: NACA-RM-L53F18a
  • Center for AeroSpace Information Number: 19930089130
  • Archival Resource Key: ark:/67531/metadc279680

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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

  • August 19, 1953

Added to The UNT Digital Library

  • March 30, 2014, 6 p.m.

Description Last Updated

  • May 24, 2018, 9:25 a.m.

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Pendley, Robert E.; Milillo, Joseph R.; Fleming, Frank F. & Bryan, Carroll R. An experimental study of five annular air inlet configurations at subsonic and transonic speeds, report, August 19, 1953; (https://digital.library.unt.edu/ark:/67531/metadc279680/: accessed May 30, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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