Marlow Anderson Field • Hobart, WA

Lake Sawyer Hawks

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Aileron Differential

Adverse yaw, especially on flat-bottom wings, is caused by the difference in airflow density between the bottom and top of the wing. The airflow along the wing’s bottom is denser than it is over the top of the wing. Therefore, the aileron moving down into this denser air creates more drag than the “up” aileron moving into the less dense airflow on top of the wing. The greater drag on just one side of the wing, the side with the down aileron, forces the wing, and the attached fuselage, to yaw in that direction. At slow airspeeds this yawing effect is more powerful, and happens faster, than the rolling effect caused by the ailerons. The airplane’s nose first swings away from the turn’s intended direction and only then begins to turn correctly once the roll begins.