سال انتشار: ۱۳۸۶
محل انتشار: پانزدهمین کنفرانس سالانه مهندسی مکانیک
تعداد صفحات: ۷
Shahverdi – Assistant professor, Islamic Azad University, Science and Research Branch, Engineering Faculty Department, Tehran, Iran
Nobari – Associate Professor, Amirkabir University of Technology, Department of Aerospace Engineering Tehran, Iran
Haddadpour – Assistant Professor, Sahrif University of Technology, Department of Aerospace Engineering Tehran, Iran
Behbahani-Nejad – Assistant Professor, Shahid Chamran University of Ahvaz , Mechanical Engineering Department Ahvaz, Iran
purposes, numerical examples are presented that demonstrate the accuracy and efficiency superiority of the present method over conventionalreduced order modeling (CROM). Also, The incorporation of thisaerodynamic model into aeroelastic flutter model are shown. Stability results are presented for critical and non-critical velocities.