

EAA Chapter 838
Batten International Airport
3333 N. Green Bay Rd.
Racine, Wisconsin 53404
262.634.7575
Get Directions to EAA 838
Email Webmaster
In a coordinated, undisturbed turn, the center of lift and the center of weight remain in line thru the vertical axis of the airplane. This is due to the action of centrifugal force. But if the turn is disrupted as by a gust of wind, the center of weight and center of lift are no longer in line. The center of weightwill try to shift in the same direction as the roll of the turn. The high wing airplane has a natural action to correct for the disruption. Since the center of weight is located below the center of lift, the weight of the airplane will try to come to rest directly under the center of lift, just like a pendulum. However, in a low wing plane, since the center of weight is above the center of lift, the weight will continue in the same direction of the roll, just like a tall mast on a ship.
When the low wing plane is in a bank, the lower wing to the inside of the turn has less of a bank angle than the higher wing on the outside of the turn. This allows the lower wing to develop more vertical lift than the higher wing. It is the developed vertical lift that will raise the lowered wing, counteracting the force of the weight to continue into the roll. The pilot is able to make simple control adjustments without over correcting.

If a gust of wind disrupts the coordinated turn. . .
Center of Lift - the horizontal line runs through the wing.

Center of Weight
Center of Weight

Center of Lift - the wings are angled up from the horizontal line through this point.
Center of weight rolls opposite to the direction of bank and will put increasing force to upright the plane.
Center of weight rolls in the same direction of bank pulling the plane further away from vertical.
The distance of each wing from the horizontal is equal so the upward lift vector is the same, with the center of weight pulling the airplane to the vertical position and stabilizing the bank.
The upper wing is further from the horizontal so the upward lift component is smaller than the lower wing. The lower wing then has greater lift pushing the airplane upright.