Effects on control effectiveness of systematically varying the size and location of trailing-edge flaps on a 45 degrees sweptback wing at a Mach number of 1.9

Author: Jacobsen, Carl R.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51I26
Link: https://digital.library.unt.edu/ark:/67531/metadc59059/

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