Gas Turbine Combustor Liner Life Assessment Using a Combined Fluid/Structural Approach

Engineering

• Fluid 100%
• Gas Turbine Combustors 100%
• Fields 50%
• Computational Fluid Dynamics 50%
• Strain 50%
• Crack Initiation 50%
• Combustor 50%
• Cycles 50%
• Computational Effort 50%
• Obtains 50%
• Fatigue Life 50%
• Temperature 50%
• Creep 50%
• Field Data 50%
• Elements 50%
• Jet Engine 50%