Prediction and experimental evaluation of planar wing spanloads for minimum drag

Keyphrases

• Root Bending Moment 100%
• Design Requirements 50%
• Relative Difference 50%
• Performance Value 50%
• Lagrange multiplier 50%
• Viscous Effects 50%
• Optimization Methods 50%
• Wind Tunnel Test 50%
• Survey Measurement 50%
• Wake Survey 50%
• Inviscid 50%
• Wing Configurations 50%
• Wind Tunnel Model 50%
• Five-hole Probe 50%
• Wing Performance 50%
• Spanwise Lift Distribution 50%
• Elliptic Wing 50%

Engineering

• Bending Moment 100%
• Relative Difference 50%
• Predicted Value 50%
• Optimization Method 50%
• Lagrange Multiplier Method 50%
• Design Constraint 50%
• Lift Distribution 50%