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The calculation of downwash behind supersonic wings with an application to triangular plan forms
Document ID
19930082279
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Heaslet, Max A
Lomax, Harvard
Date Acquired
August 16, 2013
Publication Date
June 1, 1948
Report/Patent Number
NACA-TN-1620
Report Number: NACA-TN-1620
Accession Number
93R11569
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOAD DISTRIBUTION - WINGS, SWEPTBACK
DOWNWASH
AIR FLOW - WAKES
THEORIES - WINGS SUPERSONIC
WINGS, DELTA
VORTICES
THEORIES - FLOW DOUBLETS

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