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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