Novel Parametric Reduced Order Model for Aeroengine Blade Dynamics

Engineering

• Dynamic Behavior 100%
• Reduced Order Model 100%
• Aeroengine 100%
• Frame Model 100%
• Joints (Structural Components) 50%
• Fits and Tolerances 50%
• Full Scale 50%
• Mode Shape 50%
• Turbofan Engines 50%
• Initial Configuration 50%
• Frequency Vibration 50%
• Structural Identification 50%
• Tunnel Construction 50%
• Fan Blade 50%
• Cost Function 50%
• Linear Combination 50%
• Relative Error 50%
• Resonant Frequency 50%