In this work natural complex frequencies of a flexible wing with aileron are investigated, influence of torsional vibrations of the wing on the character of flexural aileron vibrations is considered. As distinguished from work 4 the problem is solved with the help of a high speed electronic digital computer.nDetermination of critical speed and frequency is a ,well known problem of flexural and torsional vibrations of a wing with aileron, however the investigation of trajectories of complex frequencies has been covered only slightly in literature.
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