1957•Unpublished venueRequires access

Investigation of the aerodynamic characteristics in pitch and sideslip of a 45 degree swept-wing airplane configuration with various vertical locations of the wing and horizontal tail : static lateral and directional stability; Mach numbers of 1.41 a

M Leroy Spearman, Ross B Robinson

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Key concepts: Wing, Airplane, Wing twist, Wing loading, Wing configuration, Longitudinal static stability, Aerodynamics, Angle of attack

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Investigation of the aerodynamic characteristics in pitch and sideslip of a 45 degree swept-wing airplane configuration with various vertical locations of the wing and horizontal tail : static lateral and directional stability; Mach numbers of 1.41 a — Research Paper | ScholarLens