Wind-Tunnel Investigation at Subsonic and Low Transonic Speeds of the Effects of Aileron Span and Spanwise Location on the Rolling Characteristics of a Test Vehicle With Three Untapered 45 Degree Sweptback Wings

Author: Johnson, Harold S.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51B16
Link: https://digital.library.unt.edu/ark:/67531/metadc58750/

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