Tests reported are flight tests made to establish set of design and efficiency curves which were judged accurate by comparison with related wind tunnel data; propellers used were of adjustable pitch type supplied by Freedman Burnham Engineering Co, and tests were run with blade angles ranging from 8 to 28° at .75 R station. Photographs not included with mimeographed copies.
Propeller efficiency of light airplane
Soc Automotive Engrs -- Preprint
Society of Automotive Engineers -- Meeting ; 1944 Testing
1944
9 pages
9 Supp Plates, Bibliography
Conference paper
English
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