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An Investigation at Subsonic Speeds of the Rolling Effectiveness of a Small Perforated Spoiler on a Wing Having 45 Degrees of Sweepback
Document ID
19930087234
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Bandettini, Angelo
Date Acquired
August 16, 2013
Publication Date
September 15, 1952
Report/Patent Number
NACA-RM-A52G02
Report Number: NACA-RM-A52G02
Accession Number
93R16524
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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