Small engine defined as one where primary air flow rate is not more than 75 lb of air per sec at sea level static conditions; this results in various values of output of turbines at upper limit, according to type; basis for specific weight advantage and limitations on use of 3/2 or square-cube law; applications to helicopters, VTOL, trainers, drones, missiles.
Why small engines
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1957 Small
1957
19 pages
Aufsatz (Konferenz)
Englisch
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|SAE Technical Papers | 1957
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