The flutter phenomenon is the dynamic instability of elastic structures interacting with an air flow, which occurs in various aeroelastic systems. The most known type of flutter is the bending-torsional flutter of an aircraft wing, experimentally discovered and theoretically studied at the beginning of the 20th century.
With the development of aviation, flutter occurred and still occurs in other elements of aircraft, where it has been studied in much less detail due to the difficulties of both theoretical and experimental studies. This talk provides an overview of the author's work in the field of flutter of aircraft skin panels, flutter of guided missiles, flutter of blades in jet engines and gas turbines, and flutter of helicopter propeller blades.