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; abstracts in Automotive Industries v 116 n 9 May 1 1957 p 136)
Large lightweight turbojet engines
Soc Automotive Engrs -- J
Society of Automotive Engineers -- Journal ; 65 , n 10
1957
2 pages
Article (Journal)
English
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