To evaluate relative merits of small and large engines comparison is made of data from different sources confined to engines suitable for Mach number range from 2 to 3 and altitudes of 50,000 to 70,000 ft; favorable cycle characteristics established and feasibility discussed; data, based on Curtiss-Wright Turbomotor Div design activity, show that small turbine engine will inherently satisfy requirements. (see also abstract in Soc Automotive Engrs -- J v 65 n 8 July 1957 p 90-3)
Potential advancements in field of small aircraft engines
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1957 Small
1957
20 pages
Aufsatz (Konferenz)
Englisch
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POTENTIAL ADVANCEMENTS IN THE FIELD OF SMALL AIRCRAFT ENGINES
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