Purpose of tests was to determine (1) effect of power on static longitudinal stability (elevator free), (2) effect of power on elevator hinge moments (at various tab angles), and (3) effect of power on static directional stability with model operating at high and low angle of attack. Before Inst Aeronautical Sciences.
Wind-tunnel tests on low wing monoplane with propellers running
J Aeronautical Sciences
Journal of Aeronautical Sciences ; 5 , n 4
1938
7 pages
Article (Journal)
English
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Wind-tunnel tests on low wing monoplane with propellers running
Engineering Index Backfile | 1938
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