Prediction and experimental evaluation of planar wing spanloads for minimum drag

Keyphrases

• Design Requirements 100%
• Root Bending Moment 100%
• High Aspect Ratio 50%
• Relative Difference 50%
• Performance Value 50%
• Lagrange multiplier 50%
• Viscous Effects 50%
• Optimization Methods 50%
• Wingtip 50%
• Wind Tunnel Test 50%
• Survey Measurement 50%
• Wake Survey 50%
• Wing Model 50%
• Fixed Design 50%
• Wind Tunnel Model 50%
• Profile Drag 50%
• Induced Drag 50%
• Five-hole Probe 50%
• Wing Performance 50%
• Spanwise Lift Distribution 50%
• Tip Extension 50%

Engineering

• Bending Moment 100%
• Design Constraint 100%
• Tunnel 100%
• Relative Difference 50%
• High Aspect Ratio 50%
• Predicted Value 50%
• Optimization Method 50%
• Lagrange Multiplier Method 50%
• Profile Drag 50%
• Induced Drag 50%
• Fixed Design 50%
• Lift Distribution 50%