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The Dutch Roll Design &
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Dutch
Roll
Dutch roll is a combination of yawing and
rolling motion that is characteristic of all swept wing aircraft.
Disturbances about the yaw axis of an airplane will result in
disturbances about the roll axis. This is caused by the dihedral
effect of the wings (roll due to yaw). On a swept wing airplane,
this effect is due to two causes. First, when a wing with positive
dihedral (tips higher than roots) is yawed the forward wing is
at a higher angle of attack than the trailing wing. This results in
a differential lift situation which causes a rolling moment. If the
wing is also swept, the forward wing will also cause more rolling
moment than the other wing due to the greater moment arm of its
center of lift as well as the increased lift. This rolling produces
sideslip due to roll only. This sideslip on a wing with dihedral
causes a rolling moment tending to lift the down wing. The net
result is a pendulum-like motion similar to the rolling motion of a
Dutch ice speed-skater on the frozen canals of Holland, hence
the name "Dutch Roll". Loss of directional control can occur if
divergent Dutch roll is not properly damped. This is one of the
reasons for the development of yaw dampers on modern day
jets.
Source: Air Force Flight Test Center,
Edwards Air Force Base, CA
The Dutch
Roll
The Flying Dutch Girl,
Caroline
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