A 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.
Effect of Distribution of Basket-Hole Area on Simulated Altitude Performance of 25 1/2 Inch Diameter Annular-Type Turbojet Combustor
1948
52 pages
Report
No indication
English
Effect of combustor-inlet conditions on performance of Annular Turbojet Combustor
Engineering Index Backfile | 1947
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