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Wind-tunnel Investigation at Subsonic and Supersonic Speeds of a Model of a Tailless Fighter Airplane Employing a Low-aspect-ratio Swept-back Wing : Stability and Control
Document ID
19930087359
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Smith, Willard G
Date Acquired
August 16, 2013
Publication Date
January 12, 1953
Report/Patent Number
NACA-RM-A52J30
Report Number: NACA-RM-A52J30
Accession Number
93R16649
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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