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The Effect of Wing Fences on the Longitudinal Characteristics at Mach Numbers up to 0.92 of a Wing-fuselage-tail Combination Having a 40 Degree Sweptback Wing with NACA 64A Thickness Distribution
Document ID
19930088989
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dickson, Gerald K
Sutton, Fred B
Date Acquired
August 16, 2013
Publication Date
May 27, 1955
Report/Patent Number
NACA-RM-A55C30a
Report Number: NACA-RM-A55C30a
Accession Number
93R18279
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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