Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds: stability and control characteristics

Author: Hamilton, William T.
Year: 1950
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A50A03
Link: https://digital.library.unt.edu/ark:/67531/metadc64875/

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