Investigation of hinge moments of ailerons of various chords and spans on two airfoils having Clark Y and U.S.A. 27 wing sections in 10-ft. tunnel of Bureau of Standards on models of 60 in. span and 10 in. chord.
Effect of variation of chord and span of ailerons on hinge moments at several angles of pitch
Nat Advisory Committee Aeronautics -- Report
1930
15 pages
30 Figs.
Report
English
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