Engineering
Combustor
100%
High-Pressure Turbine
50%
Temperature Distribution
45%
Circumferential
42%
Flow Field
40%
Aerodynamic Performance
38%
Leading Edge
30%
Aero-Engines
28%
Numerical Study
28%
Hot Gas
28%
Turbine Inlet Temperature
21%
Machine Dynamics
21%
Turbomachinery
21%
Pressure Loss
16%
Combustion Chamber
14%
Duct
14%
Nonuniformity
14%
Boundary Layer
14%
Design Process
14%
Thermocouple
14%
Temperature Field
14%
Low-Pressure Turbine
14%
Test Bench
14%
Environmental Protection
14%
Lightweight Design
14%
Greenhouse Gas
14%
Pressure Ratio
14%
Axial Distance
14%
Experimental Investigation
14%
Cooling Air
14%
Maximum Temperature
14%
Secondary Flow
9%
Flow Structure
9%
Pressure Turbine
9%
Boundary Condition
9%
Bionics
9%
Transients
9%
Radial Position
7%