Theoretical Analysis of Effect of Aileron Inertia and Hinge Moment on Maximum Rolling Acceleration of Airplanes in Abrupt Aileron Rolls. (Advance Restricted Report Feb 1942)
Theoretical analysis of effect of aileron inertia and hinge moment on maximum rolling acceleration of airplanes in abrupt aileron rolls
Nat Advisory Committee Aeronautics -- Wartime Report
1942
13 pages
3 Supp plates
Report
English
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