Theoretical and experimental investigations of various types of aircraft (UAV's, gliders, airplanes, missiles) are carried out, including theoretical and experimental investigations of critical modes (flats), estimating the forms and frequencies of the oscillations of aircraft structural elements. Using computer simulation and experimental methods, the strength, stability and reliability characteristics of aviation and rocket structures developed from solid and composite (composite) materials are investigated.
Keywords:
Aerodynamics and Flight Dynamics
Diagnostic and measurement technologies, New materials for high-tech, Technologies for sustainable development and energy