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Investigation of a Thin Wing of Aspect Ratio 4 in the Ames 12-foot Pressure Wind Tunnel V : Static Longitudinal Stability and Control Throughout the Subsonic Speed Range of a Semispan Model of a Supersonic Airplane
Document ID
19930085990
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Johnson, Ben H , Jr
Rollins, Francis W
Date Acquired
August 16, 2013
Publication Date
December 8, 1949
Report/Patent Number
NACA-RM-A9I01
Accession Number
93R15280
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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