Force and moment test on a low boom configuration in Glenn's 8 × 6 wind tunnel

Keyphrases

• Mach number 100%
• Wind Tunnel 100%
• Low-boom 100%
• Moment Test 100%
• Force Test 100%
• Aircraft Concept 100%
• Acoustics 50%
• Reynolds number 50%
• Performance Parameters 50%
• Surface Pressure 50%
• Supersonic Wind Tunnel 50%
• Surface Rendering 50%
• Aerodynamic Stability 50%
• Aerodynamic Performance 50%
• Aerodynamic Data 50%
• Stability Parameters 50%
• Wind Tunnel Model 50%
• Visualization Data 50%
• Off-body 50%
• Experimental Aerodynamics 50%

Engineering

• Mach Number 100%
• Reynolds' Number 50%
• Experimental Investigation 50%
• NASA 50%
• Data Visualization 50%
• Aerodynamic Stability 50%
• Aerodynamic Performance 50%
• Experimental Aerodynamics 50%