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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
Author:
Bandettini, Angelo
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A52G02
Link:
https://digital.library.unt.edu/ark:/67531/metadc59337/
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