Keyphrases
Aero-engine
33%
Blade-tip Radial Running Clearance
66%
Casing Deformation
16%
Clearance Control
16%
Computational Efficiency
16%
Computational Precision
16%
Deformation Control
16%
Dynamic Optimal Control
16%
Gas Turbine
16%
High Performance
33%
High Pressure Turbine
16%
High Reliability
33%
Least Squares Support Vector Machine
100%
Material Dynamics
16%
Mathematical Model
16%
Nonlinear Dynamics
100%
Nonlinear Material Properties
16%
Numerical Experiments
16%
Optimal Control Model
16%
Optimum Control
100%
Performance Reliability
33%
Probabilistic Optimization
33%
Radial Deformation
100%
Radial Turbine
16%
Reliability Degree
16%
Support Vector Machine Model
50%
Thermal Load
16%
Turbine Casing
100%
Engineering
Aeroengine
40%
Blade Tip
80%
Computational Efficiency
20%
Control Model
20%
Design Sample
20%
Gas Turbine
20%
High-Pressure Turbine
20%
Least Square
100%
Mathematical Model
20%
Non-Linear Dynamics
100%
Numerical Experiment
20%
Optimal Control
100%
Support Vector Machine
100%
Thermal Load
20%
Turbine
100%