Theoretical comparison of several methods of thrust augmentation for turbojet engines
Description:
"A theoretical investigation of tail-pipe burning, water injection at the compressor inlet, combination tail-pipe burning plus water injection, bleedoff, and rocket-assist methods thrust augmentation for turbojet engines was made for an engine representative of those in current use. The effect of augmented liquid ratio on augmented thrust ratio and the effects of altitude and flight Mach number on the performance of various methods were determined. The additional take-off weight involved by the…
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Date:
October 27, 1948
Creator:
Hall, Eldon W. & Wilcox, E. Clinton
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department