Simulated Altitude Performance of Combustor of Westinghouse 19XB-1 Jet-Propulsion Engine Metadata
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- Main Title Simulated Altitude Performance of Combustor of Westinghouse 19XB-1 Jet-Propulsion Engine
- Series Title NACA Research Memorandums
Author: Childs, J. HowardCreator Type: Personal
Author: McCafferty, Richard J.Creator Type: Personal
Originator: Lewis Flight Propulsion LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab
- Creation: 1948-11-30
- Content Description: From Summary: "A 19XB-1 combustor was operated under conditions simulating zero-ram operation of the 19XB-1 turbojet engine at various altitudes and engine speeds. The combustion efficiencies and the altitude operational limits were determined; data were also obtained on the character of the combustion, the pressure drop through the combustor, and the combustor-outlet temperature and velocity profiles. At altitudes about 10,000 feet below the operational limits, the flames were yellow and steady and the temperature rise through the combustor increased with fuel-air ratio throughout the range of fuel-air ratios investigated. At altitudes near the operational limits, the flames were blue and flickering and the combustor was sluggish in its response to changes in fuel flow."
- Physical Description: 44 p. : ill.
- Keyword: 19XB-1
- Keyword: turbojet engines
- Keyword: aircraft combustors
Name: National Advisory Committee for Aeronautics CollectionCode: NACA
Name: Technical Report Archive and Image LibraryCode: TRAIL
Name: UNT Libraries Government Documents DepartmentCode: UNTGD
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
- URL: http://hdl.handle.net/2060/20030065290
- Report No.: NACA-RM-E8J29
- Center for AeroSpace Information Number: 20030065290
- Archival Resource Key: ark:/67531/metadc63928