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Preliminary Flight-Determined Pressure Distributions Over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers
Author:
Jordan, Gareth H.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-H55A10
Link:
https://digital.library.unt.edu/ark:/67531/metadc61198/
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