Problem of pure jet aircraft take-off distance is indicated, and basic reasons for excess thrust deficiency as compared to propeller aircraft shown; afterburner concept discussed; thrust augmentations of 45% low speed and over 100% high speed shown to be feasible; method for analyzing afterburners. (See also - discussion n 9 Sept p 521)
Afterburners for turbojet engines
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 15 , n 5
1948
7 pages
Article (Journal)
English
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