Method for Flutter Aero-servoelasti c Open

Aero-servoelasticity (ASE) is a multi-disciplinary study of interactions among structural dynamics, unsteady aerodynamics,and control systems. In this paper, the Aircraft Test Model (ATM) developed by the NASA Dryden Flight Research Center is used, and the velocities at which flutter occurs are calculated by use of the Structural Analysis Routines (STARS) aero-servoelastic For the validation of our aero-servoelastic the STARS aero-servoelastic software, also developed by NASA, is used. We developed a new aero-servoelastic tool in Matlab to consider these interactions, and the results obtained through our method are compared with the ones obtained through STARS.