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Effects of streamline curvature on lift of biplanesThis report concerns, first, the determination of the lift of a wing which is situated in a curvilinear flow; and second, to calculate the curvature which one wing of a biplane produces in the vicinity of the other.
Document ID
19930090780
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Prandtl, L
Date Acquired
September 6, 2013
Publication Date
June 1, 1927
Report/Patent Number
NACA-TM-416
Accession Number
93R20070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS, BIPLANE - LIFT
WINGS - LIFT

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