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Pressure distribution and aerodynamic loadings for several-flap-type trailing-edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
Author:
Lord, Douglas R.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55J03
Link:
https://digital.library.unt.edu/ark:/67531/metadc61789/
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