Nonlinear Aeroelastic Analysis of a Full Flexible Aircraft Using Assumed Modes Method and a Minimum-State Aerodynamic Model

Document Type : Research Article

Authors

• Salman Shafaghat ¹
• Mohammadali Noorian ²
• Reza Azarafza ³

¹ Faculty of Aerospace Engineering, Malek-Ashtar University of Technology, Tehran, Iran

² Faculty of Aerospace Engineering, K. N. Toosi University of Technology, Tehran, Iran

³ Faculty of Materials and Manufacturing Technologies, Malek-Ashtar University of Technology, Tehran, Iran

Abstract

Keywords

• Full Flexible Aircraft
• Quasi-Coordinate System
• Nonlinear Aeroelasticity
• Limit Cycle Oscillations (LCO)
• Flight Dynamic Modes

Main Subjects

• Nonlinear Vibration
• Aerospace Materials and Structure