Effects of Varying the Size and Location of Trailing-Edge Flap-Type Controls on the Aerodynamic Characteristics of a Unswept Wing at a Mach Number of 1.9

Author: Mitchell, Meade H., Jr.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L50F08
Link: https://digital.library.unt.edu/ark:/67531/metadc58483/

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