Icing-protection requirements for reciprocating-engine induction system

One of 1,423 reports in the series: NACA Technical Reports available on this site.

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Description

From Summary: "Despite the development of relatively ice-free fuel-metering systems, the widespread use of alternate and heated-air intakes, and the use of alcohol for emergency de-icing, icing of aircraft-engine induction systems is a serious problem. Investigations have been made to study and to combat all phases of this icing problem. From these investigations, criterions for safe operation and for design of new induction systems have been established. The results were obtained from laboratory investigations of carburetor-supercharger combinations, wind-tunnel investigations of air scoops, multicylinder-engine studies, and flight investigations. Characteristics of three forms of ice, impact, throttling, and fuel evaporation were studied."

Physical Description

611 - 634 p. : ill.

Creation Information

Coles, Willard D.; Rollin, Vern G. & Mulholland, Donald R. June 20, 1949.

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

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  • Main Title: Icing-protection requirements for reciprocating-engine induction system
  • Series Title: NACA Technical Reports

Description

From Summary: "Despite the development of relatively ice-free fuel-metering systems, the widespread use of alternate and heated-air intakes, and the use of alcohol for emergency de-icing, icing of aircraft-engine induction systems is a serious problem. Investigations have been made to study and to combat all phases of this icing problem. From these investigations, criterions for safe operation and for design of new induction systems have been established. The results were obtained from laboratory investigations of carburetor-supercharger combinations, wind-tunnel investigations of air scoops, multicylinder-engine studies, and flight investigations. Characteristics of three forms of ice, impact, throttling, and fuel evaporation were studied."

Physical Description

611 - 634 p. : ill.

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  • Accession or Local Control No: 93R21333
  • URL: http://hdl.handle.net/2060/19930092043 External Link
  • Report No.: NACA-TR-982
  • Center for AeroSpace Information Number: 19930092043
  • Report No.: NACA-TN-1993
  • Archival Resource Key: ark:/67531/metadc60321

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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

  • June 20, 1949

Added to The UNT Digital Library

  • Nov. 17, 2011, 5:13 p.m.

Description Last Updated

  • April 10, 2018, 12:47 p.m.

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Coles, Willard D.; Rollin, Vern G. & Mulholland, Donald R. Icing-protection requirements for reciprocating-engine induction system, report, June 20, 1949; (https://digital.library.unt.edu/ark:/67531/metadc60321/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.

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