Aerodynamic characteristics of a 60 degree delta wing having a half-delta tip control at a Mach number of 4.04

Author: Ulmann, Edward F
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L55A19
Link: https://digital.library.unt.edu/ark:/67531/metadc61308/

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