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Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds
Document ID
19930082987
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Harmon, Sidney Morris
Date Acquired
August 29, 2013
Publication Date
April 1, 1951
Report/Patent Number
NACA-TN-2344
Report Number: NACA-TN-2344
Accession Number
93R12277
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLOW, SUPERSONIC
THEORIES - FLOW
WINGS, COMPLETE - WAKE
THIN
THEORIES - AIRFOILS
WINGS,COMPLETE - THEORY
LOADS, STEADY - WINGS
WINGS, COMPLETE - SWEEP
DOWNWASH
LINEAR
FLOW, SUBSONIC
THEORIES - WINGS
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