Flight-determined static lateral stability and control characteristics of a swept-wing fighter airplane to a Mach number of 1.39

Author: Matranga, Gene J
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-H57A16
Link: https://digital.library.unt.edu/ark:/67531/metadc63030/

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