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Aerodynamic Characteristics of Two Rectangular-plan-form, Allmovable Controls in Combination With a Slender Body of Revolution at Mach Numbers From 3.00 to 6.25
Author:
Wong, Thomas J.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A55J07
Link:
https://digital.library.unt.edu/ark:/67531/metadc52886/
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