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Vane - Subsystems |
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Vane - Subsystems |
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The secondary purpose is to provide yaw control during conventional flight with the differential drag generated by extending the split flaps on one blade or the other.
This is information proprietary to
William Terry (Bill) Holmes and his heirs
756 SE Linn Street, Portland, Oregon 97202, 503-432-8577 (home),
760-917-2498, wtholmes.com, william@wtholmes.com.
No disclosure is authorized without prior written permission by
William Terry Holmes.
