Subsonic Flight Investigation Of Methods To Improve The Damping Of Lateral Oscillations By Means Of A Viscous Damper In The Rudder System In Conjuction With Adjusted Hinge Moment Parameters
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| Author | : Harold L. Crane |
| Publisher | : |
| Total Pages | : 654 |
| Release | : 1958 |
| Genre | : Airplanes |
| ISBN | : |
A flight investigation at subsonic speeds of a method to improve the damping of lateral oscillations by means of a viscous damping cylinder used in the rudder system in conjunction with adjusted hinge-moment parameters has been conducted. The damping device has been applied to a modern fighter-type jet-powered airplane. The rudder was made to float with the relative wind by the addition of trailing-edge strips. In order to amplify the floating tendency (by reducing the restoring moment), a highly geared balancing tab was incorporated. Lag of the motion of the free rudder with respect to the yawing of the airplane was introduced by means of a small viscous damping cylinder linked to the rudder.
| Author | : Harold L. Crane |
| Publisher | : |
| Total Pages | : 58 |
| Release | : 1954 |
| Genre | : Airplanes |
| ISBN | : |
A flight investigation at subsonic speeds of a method to improve the damping of lateral oscillations by means of a viscous damping cylinder used in the rudder system in conjunction with adjusted hinge-moment parameters has been conducted. The damping device has been applied to a modern fighter-type jet-powered airplane. The rudder was made to float with the relative wind by the addition of trailing-edge strips. In order to amplify the floating tendency (by reducing the restoring moment), a highly geared balancing tab was incorporated. Lag of the motion of the free rudder with respect to the yawing of the airplane was introduced by means of a small viscous damping cylinder linked to the rudder.
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1076 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 716 |
| Release | : 1956 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1698 |
| Release | : 1959 |
| Genre | : Government publications |
| ISBN | : |
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1959 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 388 |
| Release | : 1957 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : Defense Documentation Center (U.S.) |
| Publisher | : |
| Total Pages | : 894 |
| Release | : 1960 |
| Genre | : Industrial arts |
| ISBN | : |
| Author | : Harold L. Crane |
| Publisher | : |
| Total Pages | : 45 |
| Release | : 1958 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 770 |
| Release | : 1948 |
| Genre | : Mechanics, Applied |
| ISBN | : |
