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On the Minimum Induced Drag of WingsBirds do not require the use of vertical tails. They do not appear to have any mechanism by which to control their yaw. As an example the albatross is notable in this regard. The authors believe this is possible because of a unique adaptation by which there exists a triple-optimal solution that provides the maximum aerodynamic efficiency, the minimum structural weight, and it provides for coordination of control in roll and yaw. Until now, this solution has eluded researchers, and remained unknown. Here it is shown that the correct specification of spanload provides for all three solutions at once, maximum aerodynamic efficiency, minimum structural weight, and coordinated control. The implications of this result has far reaching effects on the design of aircraft, as well as dramatic efficiency improvement.
Document ID
20150009297
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Bowers, Albion H.
(NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
June 1, 2015
Publication Date
May 14, 2015
Subject Category
Aircraft Stability And Control
Aircraft Design, Testing And Performance
Report/Patent Number
DFRC-E-DAA-TN23522
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
flight mechanics
induced drag
aerodynamics
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