Preliminary Study of Some Factors which Affect the Stall-flutter Characteristics of Thin Wings
Title | Preliminary Study of Some Factors which Affect the Stall-flutter Characteristics of Thin Wings PDF eBook |
Author | A. Gerald Rainey |
Publisher | |
Pages | 38 |
Release | 1952 |
Genre | Airplanes |
ISBN |
Some of the other factors considered were found to be more or less significant however, all the factors will require further study if their effects are to be more fully interpreted.
Preliminary Study of Some Factors which Affect the Stall-flutter Characteristics of Thin Wings
Title | Preliminary Study of Some Factors which Affect the Stall-flutter Characteristics of Thin Wings PDF eBook |
Author | A. Gerald Rainey |
Publisher | |
Pages | 33 |
Release | 1956 |
Genre | Airplanes |
ISBN |
Some of the other factors considered were found to be more or less significant however, all the factors will require further study if their effects are to be more fully interpreted.
Research Abstracts and Reclassification Notice
Title | Research Abstracts and Reclassification Notice PDF eBook |
Author | United States. National Advisory Committee for Aeronautics |
Publisher | |
Pages | 508 |
Release | 1954 |
Genre | Aeronautics |
ISBN |
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
Title | 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 PDF eBook |
Author | Harold L. Crane |
Publisher | |
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.
Aircraft Propulsion Systems Technology and Design
Title | Aircraft Propulsion Systems Technology and Design PDF eBook |
Author | Gordon C. Oates |
Publisher | AIAA |
Pages | 544 |
Release | 1989 |
Genre | Aircraft gas-turbines |
ISBN | 9781600860218 |
WADC Technical Report
Title | WADC Technical Report PDF eBook |
Author | United States. Wright Air Development Division |
Publisher | |
Pages | 1268 |
Release | 1957 |
Genre | Aeronautics |
ISBN |
A Selected Listing of NASA Scientific and Technical Reports for ...
Title | A Selected Listing of NASA Scientific and Technical Reports for ... PDF eBook |
Author | |
Publisher | |
Pages | 818 |
Release | 1954 |
Genre | Aeronautics |
ISBN |