Adaptation of aeronautical engines to high altitude flying

One of 4,107 reports in the series: NACA Technical Notes available on this site.

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Description

Report discussing Issues and techniques relative to the adaptation of aircraft engines to high altitude flight. Covered here are the limits of engine output, modifications and characteristics of high altitude engines, the influence of air density on the proportions of fuel mixtures, methods of varying the proportions of fuel mixtures, the automatic prevention of fuel waste, and the design and application of air pressure regulators to high altitude flying. Summary: 1. Limits of engine output. 2. High altitude engines. 3. Influence of air density on proportions of mixture. 4. Methods of varying proportions of mixture. 5. Automatic prevention of fuel … continued below

Physical Description

30 p. : ill.

Creation Information

Kutzbach, K. May 1923.

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

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Titles

  • Main Title: Adaptation of aeronautical engines to high altitude flying
  • Series Title: NACA Technical Notes

Description

Report discussing Issues and techniques relative to the adaptation of aircraft engines to high altitude flight. Covered here are the limits of engine output, modifications and characteristics of high altitude engines, the influence of air density on the proportions of fuel mixtures, methods of varying the proportions of fuel mixtures, the automatic prevention of fuel waste, and the design and application of air pressure regulators to high altitude flying. Summary: 1. Limits of engine output. 2. High altitude engines. 3. Influence of air density on proportions of mixture. 4. Methods of varying proportions of mixture. 5. Automatic prevention of fuel waste. 6. Design and application of air pressure regulators to high altitude flying.

Physical Description

30 p. : ill.

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Identifier

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  • Accession or Local Control No: 93R10335
  • OCLC: 1100474426
  • URL: http://digital.library.unt.edu/ark:/67531/metadc53936/ External Link
  • Report No.: NACA-TN-142
  • Center for AeroSpace Information Number: 19930081045
  • Archival Resource Key: ark:/67531/metadc53936

Collections

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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).

Technical Report Archive and Image Library

The Technical Report Archive & Image Library (TRAIL) identifies, acquires, catalogs, digitizes and provides unrestricted access to U.S. government agency technical reports. The mission of TRAIL is to ensure preservation, discoverability, and persistent open access to government technical publications regardless of form or format.

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Creation Date

  • May 1923

Added to The UNT Digital Library

  • Nov. 14, 2011, 7:18 p.m.

Description Last Updated

  • Sept. 6, 2019, 3:54 p.m.

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Kutzbach, K. Adaptation of aeronautical engines to high altitude flying, report, May 1923; (https://digital.library.unt.edu/ark:/67531/metadc53936/: accessed October 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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