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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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