Publication Date:
2019-06-27
Description:
Gust-alleviation benefits for aircraft employing an unconventional wing, free to pivot about a spanwise axis forward of its aerodynamic center and subject only to aerodynamic pitching moments imposed by lift and drag forces and a trailing-edge control surface are reviewed.
Keywords:
AERODYNAMICS
Type:
NASA-CR-2046
Format:
application/pdf
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