Keyphrases
Gas Turbine Performance Simulation
100%
Vane
100%
Turbine Cooling
100%
Heat Transfer Model
100%
Coolant
75%
Mass Flow Rate
50%
Turbine Model
50%
Heat Transfer Calculation
50%
Coolant Temperature
50%
Cooling Requirements
50%
Gas Flow Field
50%
Cooled Blade
50%
Axial Resolution
50%
Performance Simulation
50%
Heat Transfer Prediction
50%
Flow Rate Measurement
50%
Cooling System
25%
Two Dimensional
25%
Web-based
25%
Design Framework
25%
Performance Results
25%
Temperature Gradient
25%
Resolution Method
25%
Two-objective
25%
Cooled Turbine
25%
Work Efficiency
25%
Simulation Program
25%
Thermodynamic Efficiency
25%
Requirement Forecasting
25%
Finite number
25%
Local Heat Transfer
25%
Multi-stage Turbine
25%
Steady-state Conditions
25%
Simulation Platform
25%
Engine Performance
25%
Cooling Method
25%
Conductive Heat Transfer
25%
Convective Heat Transfer
25%
High Usability
25%
Blade Cooling
25%
Simulation Framework
25%
High Pressure Turbine
25%
Main Flow
25%
Additional Inputs
25%
Cooling Design
25%
Metal Temperature
25%
Heat Transfer Effect
25%
Specific Fuel Consumption
25%
Blade Material
25%
Conduction Model
25%
Cooling Performance
25%
Turbine Performance
25%
Specific Thrust
25%
Dominant Effect
25%
Turbine Entry Temperature
25%
Gas Turbine Engine
25%
Engineering
Mass Flowrate
100%
Turbine Work
100%
Axial Resolution
100%
Cooling Requirement
100%
Gas Flow
100%
Gas Turbine
100%
Two Dimensional
50%
Applicability
50%
State Condition
50%
Local Heat Transfer
50%
Heat Transfer Effect
50%
Finite Number
50%
Cooling Performance
50%
Good Agreement
50%
Simulation Program
50%
Engine Performance
50%
Multistage
50%
Main Flow
50%
One Dimensional
50%
Experimental Work
50%
Main Stream
50%
High-Pressure Turbine
50%
Simulation Platform
50%
Specific Fuel Consumption
50%
Blade Cooling
50%
Gas Turbine Engine
50%
Cooling System
50%
Conductive
50%
Convective
50%
Temperature Gradients
50%