Quote:
Originally Posted by thorst
I hope to understand your question right. The yaw axis was controlled by small airbrakes far out on the wings. They could be actuated seperately on each wing, so the wing on which they were deployed is pushed back, resulting in a yaw to this side. That's how I understand it, if I'm wrong please correct me!
Thorsten
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The B-2 has split aileron that open and add drag....don't know how Horten did it.....Rich