Numerical modeling of flow and thermal patterns within a combustor simulator

Keyphrases

• 3D CFD 33%
• Air Force 33%
• CFD Analysis 66%
• Circumferential Direction 33%
• Combustor 100%
• Dilution Hole 33%
• Effect Evaluation 33%
• Exit Routes 33%
• Experimental Implementation 33%
• Film Cooling Hole 33%
• Flow Field 66%
• Flow Pattern 100%
• Gas Turbine Rotor 33%
• Heat Transfer 33%
• Heat Transfer Loss 33%
• High Turbulence 33%
• High-pressure Gas 33%
• Inlet Profiles 66%
• Liner 66%
• Mass Flow 33%
• Non-reactivity 33%
• Non-uniform Pressure 33%
• Numerical Modeling 100%
• Performance Control 33%
• Performance Enhancement 33%
• Pressure Variation 33%
• Profile Shape 33%
• Radial Direction 33%
• Secondary Flow Field 33%
• Shape Prior 33%
• Temperature Uniformity 33%
• Temperature Variation 33%
• Thermal Field 33%
• Thermal Patterns 100%
• Turbine Airfoil 33%
• Turbine Cooling 33%
• Turbine Inlet 33%
• Turbine Stage 33%
• Turbulence Level 33%
• Two-row 33%
• Vane 33%

Engineering

• Circumferential Direction 14%
• Combustor 100%
• Computational Fluid Dynamics 42%
• Cooling Hole 14%
• Desired Shape 14%
• Dilution 14%
• Exit Flow 14%
• Full Scale 14%
• Gas Turbine 14%
• Heat Losses 14%
• Numerical Modeling 100%
• Pressure Gas 14%
• Radial Direction 14%
• Rotors 14%
• Secondary Flow 14%
• Thermal Field 14%
• Turbine 100%
• Turbines Airfoil 14%