International Science and Technology Journal

In this research, the phenomenon of flutter and bending in aircraft wings was studied. In the first part, this phenomenon was defined in general, the causes leading to it, and the problems resulting from it, along with an introduction to the importance of studying it and finding appropriate solutions for it, in addition to some reference studies about it. In the second part, the explanation of the phenomenon of aeroelasticity was expanded upon, and a historical overview of its appearance and the experiments conducted on it was provided, in addition to the definition of static aeroelasticity, such as the static aeroelastic behavior of a Fixed Root Flexible Wing {the lift coefficient for 3D wing and the effect of AR on Cl versus angle of attack graph. The typical effect of a (negative) twist angle on the lift distribution. As well as the Twist Angle and its effect on the lift distribution, in addition to Twist and Divergence of the Fixed Root Flexible Wing. Dynamic Aeroelasticity is also explained: Flutter instability, Types of Flutter and the effect of spacing and wind speed on the Flutter. The third part dealt with methods of flutter control for wings and Panels, explaining some of these methods and the experiments conducted by researchers in this field. A computer simulation conducted on one of the engineering programs {MATLAB, and ANSYS} of one of the damping methods to stabilize the aircraft, avoid flutter at different speeds, and determine the best speed according to the Mach number.............. Key Words: ..............flutter, aeroelasticity, Twist, Divergence, Flutter instability, computer simulation, engineering programs, damping, aircraft.