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Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 Employing High-velocity Blowing over the Leading- and Trailing-edge Flaps
Document ID
19930089845
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Hickey, David H
Aoyagi, Kiyoshi
Date Acquired
August 16, 2013
Publication Date
May 26, 1958
Report/Patent Number
NACA-RM-A58A09
Accession Number
93R19135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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