Altitude Performance Investigation of Two Single-Annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor With Various Combustor-Inlet Air Pressure Profiles

One of 5,165 reports in the series: NACA Research Memorandums available on this site.

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Description

Report presenting data obtained three single annular-type combustors with different combustor inlet-air pressure profiles over a range of engine speeds. Results regarding effect of changing combustor inlet-air pressure profile and hole geometry on combustor performance, performance of the prototype J40-WE-8 turbojet engine combustor, correlation of combustion efficiency with engine fuel-air ratio and combustion parameter, and comparison of several combustors from different turbojet engines are provided.

Physical Description

46 p. : ill.

Creation Information

Sobolewski, Adam E.; Miller, Robert R. & McAulay, John E. May 29, 1953.

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

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  • Main Title: Altitude Performance Investigation of Two Single-Annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor With Various Combustor-Inlet Air Pressure Profiles
  • Series Title: NACA Research Memorandums

Description

Report presenting data obtained three single annular-type combustors with different combustor inlet-air pressure profiles over a range of engine speeds. Results regarding effect of changing combustor inlet-air pressure profile and hole geometry on combustor performance, performance of the prototype J40-WE-8 turbojet engine combustor, correlation of combustion efficiency with engine fuel-air ratio and combustion parameter, and comparison of several combustors from different turbojet engines are provided.

Physical Description

46 p. : ill.

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  • Accession or Local Control No: 93R16667
  • URL: http://hdl.handle.net/2060/19930087377 External Link
  • Report No.: NACA-RM-E52J07
  • Center for AeroSpace Information Number: 19930087377
  • Archival Resource Key: ark:/67531/metadc59447

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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

  • May 29, 1953

Added to The UNT Digital Library

  • Nov. 17, 2011, 10:13 p.m.

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  • July 25, 2018, 9:16 a.m.

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Sobolewski, Adam E.; Miller, Robert R. & McAulay, John E. Altitude Performance Investigation of Two Single-Annular Type Combustors and the Prototype J40-WE-8 Turbojet Engine Combustor With Various Combustor-Inlet Air Pressure Profiles, report, May 29, 1953; (https://digital.library.unt.edu/ark:/67531/metadc59447/: accessed May 19, 2019), University of North Texas Libraries, Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.