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Effects of two trailing-edge controls on the aerodynamic characteristics of a rectangular wing and body combination at Mach numbers from 3.00 and 5.05
Author:
Gloria, Hermilo R.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A55K07
Link:
https://digital.library.unt.edu/ark:/67531/metadc61900/
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