Lift augmentation of a low-aspect-ratio thick wing in ground effect

Engineering

• Aspect Ratio 100%
• Ground Effect 100%
• Leading Edge 100%
• Buckling 50%
• Pitching Moment 50%
• Wind Tunnel Test 50%
• Test Section 50%
• Bottom Surface 50%
• Tunnel Operation 50%
• Attached Flow 50%
• Calibration Curve 50%
• Diagonal Strut 50%
• Pitching Moment Coefficient 50%
• Trailing Edge 50%

Keyphrases

• Lift Augmentation 100%
• CATIA 100%
• Wing-in-ground Effect 100%
• Six-component Balance 50%
• Camber 50%
• Pitching Moment Coefficient 50%
• NC Milling 50%
• High-speed Catamaran 50%
• Tunnel Operation 50%
• Attached Flow 50%
• Diagonal Strut 50%
• Smooth Flow 50%
• Lock nut 50%