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 abstracts in Automotive Industries v 116 n 9 May 1 1957 p 136; Soc Automotive Engrs -- J v 65 n 10 Sep 1957 p 25-6)
Large lightweight turbojet engines
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1957 Design
1957
25 pages
Aufsatz (Konferenz)
Englisch
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