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Subsonic flight investigation of methods to improve the damping of lateral oscillations by means of a viscous damper in the rudder system in conjunction with adjusted hinge-moment parameters

Title:Subsonic flight investigation of methods to improve the damping of lateral oscillations by means of a viscous damper in the rudder system in conjunction with adjusted hinge-moment parameters
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Note:National Advisory Committee for Aeronautics, 1954
  
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Subject:Airplanes -- Steering-gear
Subject:Airplanes -- Tail surfaces
Subject:Damping (Mechanics)
Subject:Hinge moments (Aerodynamics)
Subject:Oscillations
Subject:Stability of airplanes, Lateral
Subject:Viscosity
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