Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft

Keyphrases

• Wind Tunnel Test 100%
• Supersonic Aircraft 100%
• Gearbox 100%
• Nacelle 100%
• Three-dimensional Flow 66%
• Sonic Boom 66%
• Protuberance 66%
• Crane Beam 66%
• Engine Model 66%
• Bypass Flow 66%
• Flow Field 33%
• Low Noise 33%
• Blockage 33%
• Attenuation 33%
• Dynamic Pressure 33%
• Computational Results 33%
• Flow Velocity 33%
• Wind Tunnel 33%
• Flow Path 33%
• Flight Condition 33%
• Design Challenges 33%
• Increasing Complexity 33%
• Pressure Measurement 33%
• Aerospace 33%
• High Flow 33%
• Surface Flow Visualization 33%
• Flow Features 33%
• Planar Maps 33%
• Total Pressure 33%
• Radial Position 33%
• Large Flow 33%
• Model Configuration 33%
• Supersonic Flight 33%
• Pressure Loss 33%
• Full Test 33%
• Bypass Model 33%
• Turbine Engine 33%
• Bypass Duct 33%
• Circumferential Angle 33%
• Recirculation Zone 33%
• Gulf Stream 33%
• Flow Recirculation 33%

Engineering

• Supersonic Aircraft 100%
• Gearbox 100%
• Axisymmetric 66%
• Sonic Boom 66%
• Bypass Flow 66%
• Flow Velocity 33%
• Flow Field 33%
• Mountings 33%
• Flow Path 33%
• Flight Condition 33%
• Dynamic Pressure 33%
• Duct 33%
• Circumferential 33%
• Surface Flow Visualization 33%
• Radial Position 33%
• Pressure Loss 33%
• Supersonic Flight 33%
• Recirculation Zone 33%