A method for nonlinear aeroelasticity trim and stability analysis of very flexible aircraft based on co-rotational theory

Engineering

• Aeroelasticity 100%
• Stability Analysis 100%
• Rotational 100%
• Flight Dynamics 66%
• Non-Linear Dynamics 66%
• Beam Element 66%
• Flexible Wings 66%
• Aerodynamics 33%
• Large Deformation 33%
• Good Agreement 33%
• Nodes 33%
• Aerodynamic Load 33%
• Response Characteristic 33%
• High Aspect Ratio 33%
• Stability Characteristic 33%
• Aerodynamic Characteristic 33%
• Mass Distribution 33%
• Stiffness Matrix 33%
• Mass Matrix 33%
• Complete Aircraft 33%