Engineering
Combustor
100%
Gas Turbine
100%
Thermal Field
100%
Field Measurement
100%
Aero-Engines
100%
Dilution
75%
Gas Turbine Engine
25%
Turbulent Flow
25%
Combustion Temperature
25%
Doppler Velocimeter
25%
Velocity Field
25%
Power Output
25%
Penetration Depth
25%
Current Demand
25%
Thermocouple
25%
Mainstream Flow
25%
Field Result
25%
Rotating Vortex
25%
Keyphrases
Combustor
100%
Flow Field
100%
Thermal Field
100%
Dilution Jets
75%
Turbulence Level
50%
High Performance
25%
Kidney
25%
Gas Turbine Engine
25%
Combustion Temperature
25%
Laser Doppler Velocimeter
25%
Velocity Field
25%
Thermocouple
25%
Power Output
25%
Penetration Depth
25%
Future Demand
25%
Additional Power
25%
Aero-engine
25%
Turbulent Flow Fields
25%
Mainstream Flow
25%
Counter-rotating Vortices
25%