// Airfoil lift (pre-stall and zero-alpha) torques "up" (negative
// torque) around the Y axis, while flap lift pushes down. Both
// forces are considered to act at one third chord from the
- // center. Convert to local (i.e. airplane) coordiantes and store
+ // edge. Convert to local (i.e. airplane) coordiantes and store
// into "torque".
torque[0] = 0;
- torque[1] = 0.33 * _chord * (flapLift - (_cz*_cz0 + stallLift));
+ torque[1] = 0.1667 * _chord * (flapLift - (_cz*_cz0 + stallLift));
torque[2] = 0;
Math::tmul33(_orient, torque, torque);