Oops, "one third from the edge" means "one SIXTH from the center".
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@ -171,10 +171,10 @@ void Surface::calcForce(float* v, float rho, float* out, float* torque)
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// Airfoil lift (pre-stall and zero-alpha) torques "up" (negative
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// torque) around the Y axis, while flap lift pushes down. Both
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// forces are considered to act at one third chord from the
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// center. Convert to local (i.e. airplane) coordiantes and store
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// edge. Convert to local (i.e. airplane) coordiantes and store
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// into "torque".
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torque[0] = 0;
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torque[1] = 0.33 * _chord * (flapLift - (_cz*_cz0 + stallLift));
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torque[1] = 0.1667 * _chord * (flapLift - (_cz*_cz0 + stallLift));
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torque[2] = 0;
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Math::tmul33(_orient, torque, torque);
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