Elevator-stabilizer effectiveness and trim of the X-1 airplane to a Mach number of 1.06

Author: Drake, Hubert M.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L50G20
Link: https://digital.library.unt.edu/ark:/67531/metadc58571/

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