An unsteady aerodynamic modeling for turbomachinery based on system identification

Engineering

• Aerodynamic Coefficient 33%
• Aerodynamic Damping 33%
• Aerodynamic Modeling 100%
• Aerodynamics 66%
• Blade Passage 33%
• Blade Row 33%
• Computational Efficiency 33%
• Computational Fluid Dynamics 66%
• Damping Coefficient 33%
• Dynamic Method 33%
• Frequency Response 33%
• Frequency Signal 33%
• Harmonics 33%
• Phase Shift 33%
• Preliminary Design 33%
• Reduced Order Model 33%
• Resonant Frequency 33%
• Small Disturbance 33%
• Stability Analysis 33%
• Superposition Principle 33%
• Sweep Frequency 66%
• Test Standard 33%
• Turbomachinery 100%