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Keyphrases
Turbine Vane
100%
Aerodynamic Loss
100%
Ceramic Matrix Composites
100%
Heat Transfer Loss
100%
Vane
50%
Reynolds number
50%
Surface Heat Transfer
33%
Boundary Layer
33%
Laminar-turbulent Transition
33%
High Efficiency
16%
Gas Turbine
16%
Smooth Surface
16%
Negative Impact
16%
Pressure Measurement
16%
Composite Materials
16%
Cycle Efficiency
16%
Surface Morphology
16%
Nusselt number
16%
Heat Transfer Enhancement
16%
Stagnation Point
16%
Infrared Measurements
16%
Linear Cascade
16%
Suction Side
16%
Random Rough Surface
16%
Turbine Heat Transfer
16%
Firing Temperature
16%
Distance Weight
16%
Boundary Layer Behavior
16%
Composite Surface
16%
Cooling Requirements
16%
Allowable Temperature
16%
Wake Losses
16%
Weave Pattern
16%
Engineering
Aerodynamics
100%
Turbine
100%
Reynolds' Number
60%
Boundary Layer
60%
Heat Transfer Surface
40%
Linear Scale
20%
Gas Turbine
20%
Smooth Surface
20%
Cycle Efficiency
20%
Nusselt Number
20%
Surface Morphology
20%
Negative Impact
20%
Suction Side
20%
Firing Temperature
20%
Cooling Requirement
20%
Composite Material
20%
Stagnation Point
20%
Laminar-Turbulent Transition
20%
Random Rough Surface
20%
Critical Micelle Concentration
20%