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On the Minimum Induced Drag of WingsPrandtl 1933 spanload development showing the wing developed to achieve this spanload, including the planform and the twist. Additionally, the derivative propeller, rotor, fan are also shown, including the planform and the twist.
Document ID
20180006672
Acquisition Source
Armstrong Flight Research Center
Document Type
Presentation
Authors
Bowers, Albion H. (NASA Armstrong Flight Research Center Edwards, CA, United States)
Date Acquired
October 24, 2018
Publication Date
August 31, 2018
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AFRC-E-DAA-TN60613
Report Number: AFRC-E-DAA-TN60613
Meeting Information
Meeting: Annual Experimental Soaring Association Western Workshop
Location: Tehachapi, CA
Country: United States
Start Date: August 31, 2018
End Date: September 3, 2018
Sponsors: Soaring Society of America
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
wing theory

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