
Разработаны математическая модель и программный комплекс моделирования сопряженных газодинамических процессов и процессов деформирования элементов конструкций. Проведены исследования процесса колебаний лопастей высокоскоростного летательного аппарата.
The mathematical model and simulation software system coupled dynamic processes and the processes of deformation of structural elements. The investigations of the process of high-speed blade vibrations of the aircraft.
АЭРОУПРУГОСТЬ,ЛЕТАТЕЛЬНЫЙ АППАРАТ,ФЛАТТЕР,КРИТИЧЕСКАЯ СКОРОСТЬ ФЛАТТЕРА,AEROELASTICITY,AIRCRAFT FLUTTER,FLUTTER CRITICAL VELOCITY
АЭРОУПРУГОСТЬ,ЛЕТАТЕЛЬНЫЙ АППАРАТ,ФЛАТТЕР,КРИТИЧЕСКАЯ СКОРОСТЬ ФЛАТТЕРА,AEROELASTICITY,AIRCRAFT FLUTTER,FLUTTER CRITICAL VELOCITY
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