Investigations into the vibrational response of an aero-engine turbine blade under thermosonic excitation

Physics

• Engine 100%
• Turbine 100%
• Responses 100%
• Vibration 80%
• Position (Location) 40%
• Frequencies 40%
• Defects 40%
• Detection 20%
• Nondestructive Test 20%
• Steady State 20%
• Displacement 20%
• Spectra 20%
• Area 20%
• Correlation 20%
• Model 20%
• Computer Aided Design 20%
• Cracks 20%
• Laser 20%
• High Pressure 20%

Material Science

• Defect 40%
• Finite Element Methods 40%
• Laser 20%
• Crack 20%
• Correlation 20%
• Non-Destructive Testing 20%

Engineering

• Forcing Function 20%
• Turbofan Engines 20%
• Detection Threshold 20%
• Pressure Compressor 20%