Advantages due to use of controllable pitch; conditions which make its use essential; effect of altitude; take-off improvements of from 50 to 100% noticed in cases where throttle stop must be used when operating at sea level; cruising at altitude; fuel economy; engine cranking while flying; range of pitch; conclusions. Before Soc Automotive Engrs. (see also Aeroplane v 47 n 1218 Sept 26 1934 p 370-2)
Effect of pitch control
West Flying
Western Flying ; 14 , n 7
1934
3 pages
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1934
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