Experimental evaluation of an inlet profile generator for high-pressure turbine tests

Keyphrases

• Combustor 100%
• Inlet Profiles 100%
• High Pressure Turbine 100%
• Turbine Inlet 66%
• Research Laboratories 33%
• Temperature Profile 33%
• Air Force 33%
• Flow Field 33%
• Heat Transfer 33%
• Aerodynamics 33%
• Gas Turbine 33%
• Thermal Field 33%
• Inlet Conditions 33%
• Pressure Profile 33%
• Profile Shape 33%
• Aircraft Engine 33%
• Turbulence 33%
• Aerodynamic Loss 33%
• Turbulence Intensity 33%
• Flow Interaction 33%
• Combustion Chamber 33%
• Altered Flow 33%
• Verification Testing 33%
• Non-reacting 33%
• Turbine Passage 33%
• Heat Transfer Loss 33%
• Flow Distribution 33%
• Combustor Geometry 33%
• Flow Physics 33%

Engineering

• High-Pressure Turbine 100%
• Profile Generator 100%
• Turbine 100%
• Combustor 50%
• Aerodynamics 25%
• Flow Distribution 25%
• Research Laboratories 12%
• Test Section 12%
• Length Scale 12%
• Field Condition 12%
• Gas Turbine 12%
• Thermal Field 12%
• Spatial Variation 12%
• Aircraft Engine 12%
• Turbulence Intensity 12%
• Pressure Profile 12%
• Engine Designer 12%
• Flow Physic 12%
• Combustion Chamber 12%
• Temperature Profile 12%