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Investigation of the Effect of Balancing Tabs on the Hinge-Moment Characteristics of a Trailing-Edge Flap-Type Control on a Trapezoidal Wing at a Mach Number of 1.61
Author:
Lord, Douglas R.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54F22
Link:
https://digital.library.unt.edu/ark:/67531/metadc60621/
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