Fan performance scaling with inlet distortions

Engineering

• Metrics 100%
• Fan Performance 100%
• Rotors 40%
• Length Scale 20%
• Incompressible Flow 20%
• Stagnation Pressure 20%
• Flow Mechanism 20%
• Continuous Operation 20%
• Do Model 20%
• Boundary Layer 20%
• Relative Location 20%
• Source Term 20%
• Blade Row 20%
• Blade Geometry 20%
• Design Flow 20%
• Stagnation Temperature 20%
• Transonic Flow 20%
• Flow Distribution 20%
• Flow Coefficient 20%
• Turboprop Engine 20%
• Diffusion Factor 20%
• Term Approach 20%

Keyphrases

• Diffusion Metrics 100%
• Turboprop Engine 33%
• Stagnation Temperature 33%
• Diffusion Factor 33%
• Pressure-swirl 33%
• Distorted Inflow 33%
• Stator Blade 33%
• Metric Scale 33%
• Boundary Layer Ingesting 33%
• Low-speed Axial Fans 33%