Observed Acoustic and Aeroeleastic Spectral Responses of a MOD-2 Turbine Blade to Turbulence Excitation

Engineering

• Spectral Response 100%
• Blade Turbine 100%
• Rotor Diameter 50%
• Ground Level 50%
• Strain Gage 50%
• Normal Force 50%
• Acoustic Pressure 50%
• Designed Experiment 50%
• Inflow Turbine 50%
• Transfer Function 50%
• Pressure Standard 50%
• Pressure Sensor 50%
• Pressure Distribution 50%