1. Bending-torsional vibrations of aircraft wing
- Author
-
Khudayarov B. A., Ruzmetov K. Sh., Turaev F. Zh., Komilova Kh. M., and Kuralov B. A.
- Subjects
Environmental sciences ,GE1-350 - Abstract
The problems of bending-torsional flutter of an aircraft wing are considered. Using equations of motion by the Bubnov-Galerkin method, based on the polynomial approximation of deflections and angle of twist, the problem is reduced to studying a system of ordinary integro-differential equations, where the independent variable is time. The solution of integro-differential equations with singular kernels is found by a numerical method based on quadrature formulas. The influence of physical-mechanical and geometric parameters on the flutter of the aircraft wing was studied. It was established that an account for the viscoelastic properties of the material of thin-walled aircraft structures leads to a 40-60% decrease in the critical flutter velocity. It is shown that an increase in the elongation parameter of an aircraft wing leads to a decrease in the flutter velocity.
- Published
- 2023
- Full Text
- View/download PDF