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Free-flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of Several Aileron Configurations on a Tapered Wing Having 42.7 Degrees Sweepback
Document ID
19930085626
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sandahl, Carl A
Date Acquired
August 16, 2013
Publication Date
January 11, 1949
Report/Patent Number
NACA-RM-L8K23
Accession Number
93R14916
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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