A reduced order modeling technique for mistuned bladed disks

Engineering

• Localization 100%
• Reduction 50%
• Engineering Structure 50%
• Rotors 50%
• Models 50%
• Mode of Vibration 50%
• Degree of Freedom 50%
• Parameter Model 50%
• Turbomachinery 50%
• Minimum Number 50%
• Finite Element Method 50%
• Lumped Parameter 50%