A COMPREHENSIVE FRAMEWORK FOR THE COUPLED NONLINEAR AEROELASTIC AND FLIGHT DYNAMIC ANALYSES OF HIGHLY FLEXIBLE AIRCRAFT

Engineering

• Flight Dynamics 100%
• Air Flow 66%
• Aerodynamics 33%
• Time Domain 33%
• Aerodynamic Load 33%
• Aeroelasticity 33%
• Structural Model 33%
• Structural Dynamics 33%
• Rotational 33%
• Aerodynamic Model 33%
• Corrector 33%
• Spatial Distribution 33%
• Bernoulli Beam 33%
• Endpoint 33%
• Stiffness Matrix 33%
• Mass Matrix 33%
• Discrete Gust 33%
• Conceptual Design Phase 33%
• Euler Angle 33%
• Preliminary Design Phase 33%
• Ground Body 33%