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Is applicable the rudder's side force and yawing moment. The force (side) created by the rudder times its length from the CG is equal to the moment. For some reason standard aerodynamics uses the wing span as the reference length. | Is applicable the rudder's side force and yawing moment. The force (side) created by the rudder times its length from the CG is equal to the moment. For some reason standard aerodynamics uses the wing span as the reference length. | ||
{{JSBSim}} | {{JSBSim}} | ||
== See also == | |||
[[Aero input and outputs]] |
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