Investigation of aerodynamic characteristics in pitch and sideslip of a 45 degree sweptback-wing airplane model with various vertical locations of wing and horizontal tail : static longitudinal stability and control, M = 2.01

Author: Spearman, M. Leroy
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L55L06
Link: https://digital.library.unt.edu/ark:/67531/metadc62064/

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