EXPERIMENTAL INVESTIGATIONS OF AN AEROELASTIC WIND TUNNEL MODEL FOR TAIL BUFFETING ANALYSIS

Keyphrases

• Aeroelasticity 100%
• Wind Tunnel Model 100%
• Horizontal Tail Plane 100%
• Tail Buffeting 100%
• Buffeting Analysis 100%
• Tailplane 66%
• Force Measurement 33%
• Accelerometer 33%
• Dynamic Excitation 33%
• Structural Dynamics 33%
• Munich 33%
• Technical University 33%
• Structural Damage 33%
• Measured Signal 33%
• Fluid Mechanics 33%
• Modular Model 33%
• Aerodynamics 33%
• Aircraft Design 33%
• Frequency Content 33%
• Vertical Tail 33%
• Fuselage 33%
• Unsteady Pressure 33%
• Handling Qualities 33%
• Model Configuration 33%
• Aerodynamic Characteristics 33%
• Aerodynamic Coefficients 33%
• Lifting Surface 33%
• High Agility 33%
• Deflection Angle 33%
• High Angle of Attack 33%
• Aeroelastic Phenomena 33%
• Structural Elasticity 33%
• Burst Size 33%
• Polylactide 33%
• Moment Measurement 33%
• Vortex Bursting 33%
• Future Aircraft 33%
• Pressure Transducer 33%
• Unsteady Flow Field 33%
• Tail Fin 33%
• Full-span Model 33%
• Span-based Model 33%
• High Turbulence Intensity 33%

Engineering

• Experimental Investigation 100%
• Tunnel 100%
• Reference Case 33%
• Structural Dynamics 33%
• Structural Damage 33%
• Angle-of-Attack 33%
• Measurement Signal 33%
• Vortex 33%
• Unsteady Flow 33%
• Turbulence Intensity 33%
• Aerodynamic Characteristic 33%
• Fluid Mechanics 33%
• Aerodynamic Coefficient 33%
• Lifting Surface 33%
• Frequency Content 33%
• Pressure Sensor 33%
• Flow Distribution 33%
• Controllability 33%
• Aerodynamics 33%