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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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