Inlet Flow Distortion in an Advanced Civil Transport Boundary Layer Ingesting Engine Installation

Keyphrases

• Inlet Distortion 100%
• Propulsor 100%
• Transport Boundaries 100%
• Boundary Layer Ingesting 100%
• Flow Field 33%
• Velocity Distribution 33%
• Stagnation Pressure 33%
• Vortex Structure 33%
• Pressure Distribution 33%
• Flow Variation 33%
• Angle of Attack 33%
• Airframe 33%
• Operating Point 33%
• Scale Model 33%
• Flow Features 33%
• Three-dimensional Flow 33%
• Propulsion System 33%
• Cruise 33%
• Qualitative Change 33%
• Nozzle Exit 33%
• Force Measurement 33%
• Quantitative Change 33%
• Twin-engine 33%
• Aircraft Configuration 33%
• Propulsive Power 33%
• Flow Uniformity 33%
• Moment Measurement 33%
• Distorted Inflow 33%
• Boundary Layer Ingestion 33%
• Double Bubble 33%

Engineering

• Boundary Layer 100%
• Propulsor 100%
• NASA 66%
• Stagnation Pressure 33%
• Vortex 33%
• Metrics 33%
• Dimensional Flow 33%
• Angle-of-Attack 33%
• Airframe 33%
• Streamwise 33%
• Propulsion System 33%
• Ducted Fan 33%
• Nozzle Exit 33%
• Operating Point 33%
• Nonuniformity 33%
• Exit Plane 33%
• Flow Distribution 33%
• Pressure Distribution 33%
• Scale Model 33%
• Tunnel 33%