Analysis of deformation of mistuned bladed disk with friction and random crystal anisotropy orientation using gradient-based polynomial chaos

Engineering

• Material Anisotropy 100%
• Gas Turbine Engine 50%
• Input Parameter 50%
• Dimensionality 50%
• System Response 50%
• Design Parameter 50%
• Blade Root 50%
• Gradient Information 50%
• Model Fidelity 50%
• Contact Condition 50%
• High-Pressure Turbine 50%
• Centrifugal Load 50%