Static longitudinal and lateral stability and control characteristics of a model of a 35 degree swept-wing airplane at a Mach number of 1.41

Author: Palazzo, Edward B.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54G08
Link: https://digital.library.unt.edu/ark:/67531/metadc60780/

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