Wind-Tunnel Tests of a 0.16-Scale Model of the Douglas MX-656 Airplane at High Subsonic Speeds, 1, Stability and Control Characteristics

Author: Hamilton, William T.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SA9D26
Link: https://digital.library.unt.edu/ark:/67531/metadc65232/

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