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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