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Effect of Distribution of Basket-Hole Area on Simulated Altitude Performance of 25 1/2-Inch-Diameter Annular-Type Turbojet CombustorA simulated altitude performance of a 25 1/2-inch-diameter annular-type turbojet combustor was performed to determine the effect of the distribution of basket-hole area on the altitude operational limits of the engine as imposed by the combustor.Total pressure drop was recorded, as well as the effect of fuel-nozzle flow capacity,and fuel-nozzle spray angle for one basket configuration. General observations were made for all configurations regarding flames, extent of afterburning, and durability of the baskets.
Document ID
20030064029
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Olson, Walter T. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Schroeter, Thomas T. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 24, 1948
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-E8A02
Report Number: NACA-RM-E8A02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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