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Line-vortex theory for calculation of supersonic downwash
Document ID
19930082603
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mirels, Harold
Haefeli, Rudolph C
Date Acquired
August 29, 2013
Publication Date
August 1, 1949
Report/Patent Number
NACA-TN-1925
Accession Number
93R11893
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS
THEORIES - AIRFOILS
UPWASH
THEORIES - WINGS
WINGS, RECTANGULAR
DOWNWASH
VORTICES, HORSEHOE
LIFTING-LINE
THEORIES - VORTEX
SUPERSONIC

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