Effect of ambient-temperature variation on the matching requirements of inlet-engine combinations at supersonic speeds

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Description

Report presenting an analysis of the effect of ambient temperature on the matching requirements of inlet-engine combinations for two typical turbojet engines up to Mach number 3.5. The results indicated that if a bypass or movable compression surface are to be used for efficient inlet-engine matching, the inlet should be sized for the lowest ambient temperature to be encountered.

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16 p.

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Perchonok, Eugene & Hearth, Donald P. January 1957.

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

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  • Main Title: Effect of ambient-temperature variation on the matching requirements of inlet-engine combinations at supersonic speeds
  • Series Title: NACA Technical Notes

Description

Report presenting an analysis of the effect of ambient temperature on the matching requirements of inlet-engine combinations for two typical turbojet engines up to Mach number 3.5. The results indicated that if a bypass or movable compression surface are to be used for efficient inlet-engine matching, the inlet should be sized for the lowest ambient temperature to be encountered.

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16 p.

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  • Accession or Local Control No: 93R13855
  • URL: http://hdl.handle.net/2060/19930084565 External Link
  • Report No.: NACA-TN-3834
  • Center for AeroSpace Information Number: 19930084565
  • Archival Resource Key: ark:/67531/metadc56081

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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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  • January 1957

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • April 17, 2018, 10:43 a.m.

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Perchonok, Eugene & Hearth, Donald P. Effect of ambient-temperature variation on the matching requirements of inlet-engine combinations at supersonic speeds, report, January 1957; (https://digital.library.unt.edu/ark:/67531/metadc56081/: accessed April 16, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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