Performance of engines in both subsonic and supersonic flight in relation to aircraft requirements; advantages and disadvantages of bypass engines and small turbojet in relation to large straight jet engine of 18,000-lb thrust: improvement in thrust/weight ratio of large engines made possible by use of titanium, and potentialities of ejector nozzles and turbine blade cooling. (See also Soc Automotive Engrs -- Paper n 81 Apr 2-5 1957 25 p; Soc Automotive Engrs -- J v 65 n 10 Sept 1957 p 25-6)
Large lightweight turbojet engines
Automotive Industries
Automotive Industries ; 116 , n 9
1957
136 pages
Article (Journal)
English
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