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Investigation of wing-tip ailerons on a 51.3 degrees sweptback wing at transonic speeds by the transonic-bump method
Document ID
19930086935
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moseley, William C , Jr
Watson, James M
Date Acquired
August 16, 2013
Publication Date
November 26, 1951
Report/Patent Number
NACA-RM-L51H27
Report Number: NACA-RM-L51H27
Accession Number
93R16225
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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