DATA FUSION UNSTEADY AERODYNAMIC MODELING BASED ON EXPERIMENTAL DATA

Engineering

• Computational Fluid Dynamics 100%
• Aerodynamic Modeling 100%
• Aerodynamics 66%
• Network Model 66%
• Airfoil 66%
• Angle-of-Attack 66%
• Test Data 66%
• Simulation Result 33%
• Time Domain 33%
• Wind Tunnel Test 33%
• Lift Coefficient 33%
• Moment Coefficient 33%
• Pitch Angle 33%
• Data Source 33%