This is the way the KR works:



Differential aileron deflection


 <http://en.m.wikipedia.org/wiki/File:DifferentialAileron.svg>
http://upload.wikimedia.org/wikipedia/en/thumb/3/3a/DifferentialAileron.svg/
450px-DifferentialAileron.svg.png

Illustration of a Differential aileron

The geometry of most aileron linkages can be configured so as to bias the
travel further upward than downward. By excessively deflecting the upward
aileron, profile drag is increased rather than reduced and separation drag
<http://en.m.wikipedia.org/wiki/Flow_separation>  further aids in producing
drag on the inside wing, producing a yaw force in the direction of the turn.
Though not as efficient as rudder mixing, aileron differential is very easy
to implement on almost any airplane and offers the significant advantage of
reducing the tendency for the wing to stall
<http://en.m.wikipedia.org/wiki/Stall_(flight)>  at the tip first by
limiting the downward aileron deflection and its associated effective
increase in angle of attack.

Most airplanes use this method of adverse yaw mitigation due to the simple
implementation and safety benefits.





See N64KR at  <http://krbuilder.org/> http://KRBuilder.org - Then click on
the pics 



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Daniel R. Heath - Lexington, SC







-----Original Message-----



Here's a good wiki on the subject.



 <http://en.m.wikipedia.org/wiki/Adverse_yaw>
http://en.m.wikipedia.org/wiki/Adverse_yaw



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