Altitude-wind-tunnel investigation of J47 turbojet-engine performance

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Description

From Introduction: "Data are presented in graphical form to show the engine performance over a range of altitudes from 5000 to 50,000 feet and flight Mach numbers from 0.21 to 0.97. Curves are presented to show the windmilling characteristics of the engine. All engine performance data obtained in the investigation are also presented in tabular form."

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44 p. : ill.

Creation Information

Conrad, E. William & Sobolewski, Adam E. November 15, 1949.

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

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From Introduction: "Data are presented in graphical form to show the engine performance over a range of altitudes from 5000 to 50,000 feet and flight Mach numbers from 0.21 to 0.97. Curves are presented to show the windmilling characteristics of the engine. All engine performance data obtained in the investigation are also presented in tabular form."

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44 p. : ill.

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  • Accession or Local Control No: 93R23083
  • URL: http://hdl.handle.net/2060/19930093773 External Link
  • Report No.: NACA-RM-E9G09
  • Center for AeroSpace Information Number: 19930093773
  • Archival Resource Key: ark:/67531/metadc62793

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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

  • November 15, 1949

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • June 7, 2018, 10:40 a.m.

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Conrad, E. William & Sobolewski, Adam E. Altitude-wind-tunnel investigation of J47 turbojet-engine performance, report, November 15, 1949; (digital.library.unt.edu/ark:/67531/metadc62793/: accessed December 16, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.