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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