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Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well Above the Wing Plane-lateral and Directional Stability
Document ID
19930088409
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wetzel, Benton E
Date Acquired
August 16, 2013
Publication Date
April 28, 1955
Report/Patent Number
NACA-RM-A54H26b
Report Number: NACA-RM-A54H26b
Accession Number
93R17699
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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