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
© Metadata Copyright Elsevier B. V. All rights reserved.
TIBKAT | 1978
|SAE Technical Papers | 1968
|Engineering Index Backfile | 1933
Engineering Index Backfile | 1930
|SAE Technical Papers | 1957
|