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The Calculation of Downwash Behind Wings of Arbitrary Plan Form at Supersonic Speeds
Document ID
19930082757
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Martin, John C
Date Acquired
August 16, 2013
Publication Date
July 1, 1950
Report/Patent Number
NACA-TN-2135
Report Number: NACA-TN-2135
Accession Number
93R12047
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOAD DISTRIBUTION, WING-SPAN
VORTICES - WINGS
THEORIES - FLOW - LINEAR
THEORIES - AIRFOILS - LIFTING-LINE
DOWNWASH
THEORIES - FLOW - SUPERSONIC
WINGS, RECTANGULAR
VORTICES, HORSESHOE
WINGS, THIN
LOAD DISTRIBUTION - TAIL SURFACES

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