Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines

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Description

Memorandum presenting hypothetical two-spool nuclear-powered turbojet engines with sea-level static design compressor total-pressure ratios of 20, 15, and 9 and total-pressure losses between the inner-spool compressor exit and turbine inlet of 10 and 30 percent. Results regarding compressor operating lines, gas-generator performance, engine performance, and some general remarks are provided.

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46 p.

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Dugan, James F., Jr. April 10, 1955.

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

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  • Main Title: Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines
  • Series Title: NACA Research Memorandums

Description

Memorandum presenting hypothetical two-spool nuclear-powered turbojet engines with sea-level static design compressor total-pressure ratios of 20, 15, and 9 and total-pressure losses between the inner-spool compressor exit and turbine inlet of 10 and 30 percent. Results regarding compressor operating lines, gas-generator performance, engine performance, and some general remarks are provided.

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46 p.

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  • Accession or Local Control No: 93R18196
  • URL: http://hdl.handle.net/2060/19930088906 External Link
  • Report No.: NACA-RM-E55K04
  • Center for AeroSpace Information Number: 19930088906
  • Archival Resource Key: ark:/67531/metadc61676

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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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  • April 10, 1955

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • Dec. 5, 2018, 10:31 a.m.

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Dugan, James F., Jr. Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines, report, April 10, 1955; (https://digital.library.unt.edu/ark:/67531/metadc61676/: accessed June 10, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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