Wind tunnel tests to determine effect of wing-tip shape and dihedral on aerodynamic characteristics of Clark Y wings affecting performance and lateral stability of airplanes; force tests at several angles of yaw and rotation tests at zero yaw; rates of change of rolling-moment, yawing-moment, and cross-wind force coefficients with angle of yaw and rate of change of rolling-moment coefficient with rolling. (Price 5c.)
Effect of tip shape and dihedral on lateral-stability characteristics
Nat Advisory Committee Aeronautics -- Report
1935
10 pages
Bibliography
Report
English
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