Simple method devised by which effect of wing elasticity on effective dihedral and on derivative in rolling moment coefficient due to sideslip may readily be determined for wings of various aspect ratios and taper ratios when different shapes of bending deflection curve are assumed.
Effect of wing bending deflection on rolling moment due to sideslip
Nat Advisory Committee Aeronautics -- Tech Note
1948
18 pages
Report
Englisch
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