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Experimental downwash and wake characteristics at subsonic and supersonic Mach numbers behind an unswept, tapered wing, of aspect ratio 2.67 with leading-and trailing-edge flaps
Document ID
19930086517
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Stivers, Louis S , Jr
Walker, Harold J
Beard, Luther, Jr
Date Acquired
August 16, 2013
Publication Date
April 21, 1951
Report/Patent Number
NACA-RM-A51B16
Report Number: NACA-RM-A51B16
Accession Number
93R15807
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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