Aerodynamic Characteristics of Two All-Movable Wings Tested in the Presence of a Fuselage at a Mach Number of 1.9

Author: Conner, D. William
Year: 1948
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L8H04
Link: https://digital.library.unt.edu/ark:/67531/metadc64577/

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