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Tests in the Ames 40- by 80-foot Wind Tunnel of an Airplane Model with an Aspect Ratio 4 Triangular Wing and an All-movable Horizontal Tail - High-lift Devices and Lateral Controls
Document ID
19930087386
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Franks, Ralph W
Date Acquired
August 16, 2013
Publication Date
February 20, 1953
Report/Patent Number
NACA-RM-A52K13
Report Number: NACA-RM-A52K13
Accession Number
93R16676
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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