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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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