High-Altitude Performance of an Experimental Turbojet Combustor Having Variable Primary-Air Admission
Description:
Report presenting an investigation of 47 experimental tubular designs embodying variable primary-air openings to control the fuel-air ratio in the combustion zone at simulated high-altitude operating conditions for a representative 5.2-pressure-ratio engine. The performance characteristics considered were combustion efficiency, operating range, and pressure loss. Results regarding the effect of fuel injector design, effect of primary-air baffles, and performance characteristics of the best mode…
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Date:
April 11, 1955
Creator:
Straight, David M. & Gernon, J. Dean
Item Type:
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