Pt 1: Flutter of wing with locked aileron; oscillations in still air and in wind; graphic representation of cycles; elimination of cycles; aerodynamic couplings; inertial couplings; inertial conditions for "semi-rigid" wing. Pt 2: Flutter of wing with unlocked aileron; conditions for effective replacement of mechanical aileron locking; elimination of aerodynamic and inertial hinge moment; inertial conditions for semirigid wing and rigid aileron.
Simple approach to wing flutter problem
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 37 , n 273
1933
10 pages
Aufsatz (Zeitschrift)
Englisch
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