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The Effect of End Plates on Swept Wings at Low Speed
Document ID
19930082868
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Riebe, John M
Watson, James M
Date Acquired
August 16, 2013
Publication Date
November 1, 1950
Report/Patent Number
NACA-TN-2229
Report Number: NACA-TN-2229
Accession Number
93R12158
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGS - END PLATES
WIND TUNNEL TESTS - NACA - 300 MPH (10 FEET X 7 FEET)
WINGS, SWEPTBACK - STABILITY
AILERONS, SPOILER
WINGS - DIHEDRAL
WINGS, SWEPTBACK - CHARACTERISTICS
AILERONS
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