Flight determination of the pressure recovery and drag characteristics of a twin side-inlet model at transonic speeds

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Description

Report presenting free-flight and free-jet testing of a twin side-inlet configuration, including a pilot's canopy and a wheel-well fairing, between a range of Mach numbers from 0.8 to 1.55. Using side inlets provides two important advantages: the inlet can be located closer to the engine and it frees up the nose for other uses. Results regarding the effects of oscillating flow, external-drag coefficient, and total-pressure recovery are provided.

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Carter, Howard S. & Merlet, Charles F. July 30, 1953.

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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 20 times . More information about this report can be viewed below.

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  • Main Title: Flight determination of the pressure recovery and drag characteristics of a twin side-inlet model at transonic speeds
  • Series Title: NACA Research Memorandums

Description

Report presenting free-flight and free-jet testing of a twin side-inlet configuration, including a pilot's canopy and a wheel-well fairing, between a range of Mach numbers from 0.8 to 1.55. Using side inlets provides two important advantages: the inlet can be located closer to the engine and it frees up the nose for other uses. Results regarding the effects of oscillating flow, external-drag coefficient, and total-pressure recovery are provided.

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  • Accession or Local Control No: 93R16868
  • URL: http://hdl.handle.net/2060/19930087578 External Link
  • Report No.: NACA-RM-L53E05
  • Center for AeroSpace Information Number: 19930087578
  • Archival Resource Key: ark:/67531/metadc59604

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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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  • July 30, 1953

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • March 28, 2018, 2:56 p.m.

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Carter, Howard S. & Merlet, Charles F. Flight determination of the pressure recovery and drag characteristics of a twin side-inlet model at transonic speeds, report, July 30, 1953; (digital.library.unt.edu/ark:/67531/metadc59604/: accessed December 10, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.