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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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