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Wind-tunnel investigation of several factors affecting the performance of a high-speed pursuit airplane with air-cooled radial engine
Document ID
19820069268
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wenzinger, C. J.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
September 4, 2013
Publication Date
November 1, 1941
Subject Category
Aerodynamics
Report/Patent Number
NACA-SR-211
Accession Number
82N74537
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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