Pt 1: Propulsive characteristics of 2-and 3-bladed adjustable pitch propellers extended to fairly large blade angles; tip loss; blade deflection; wind tunnel wall interference. Pt 2: Airplane characteristics as affected by operation of propulsive system; experimental results and analysis of effect of power on lift, drag, performance, pitching moment, longitudinal stability, and elevator effectiveness.
Wind tunnel tests on high wing monoplane with running propeller
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 3 , n 3
1936
13 pages
Article (Journal)
English
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Wind tunnel tests on a model of a monoplane wing with floating ailerons
Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929