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Aerodynamic Characteristics of Two All-Movable Wings Tested in the Presence of a Fuselage at a Mach Number of 1.9
Author:
Conner, D. William
Year:
1948
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L8H04
Link:
https://digital.library.unt.edu/ark:/67531/metadc64577/
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