Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow /

The investivation is made for thin flate-plate wings for steady vertical and longitudinal motions, setady rolling and pitching, and motions in which the wing is accelerating uniformly in the vertical direction.This report contains an investigation by means of the linearized theory to obtain relations between the stability derivatives of a wing and its reverse in supersonic flow. The wings investigated have a supersonic leading edge, a supersonic trailing edge, and either supersonic side edges or a subsonic nonre-entrant side edges which are noninteracting.NACA TN No. 1943."September 1949."Includes bibliographical references.The investivation is made for thin flate-plate wings for steady vertical and longitudinal motions, setady rolling and pitching, and motions in which the wing is accelerating uniformly in the vertical direction.This report contains an investigation by means of the linearized theory to obtain relations between the stability derivatives of a wing and its reverse in supersonic flow. The wings investigated have a supersonic leading edge, a supersonic trailing edge, and either supersonic side edges or a subsonic nonre-entrant side edges which are noninteracting.Mode of access: Internet