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The Aerodynamic Design of Wings with Cambered Span Having Minimum Induced DragAerodynamic design of wings with cambered span having minimum induced drag
Document ID
19640006060
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Cone, C. D., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1963
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TR-R-152
Accession Number
64N15974
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CAMBERED WING
AERODYNAMICS
DRAG

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