| Author | : Dennis J. Martin |
| Publisher | : |
| Total Pages | : 20 |
| Release | : 1951 |
| Genre | : Flutter (Aerodynamics) |
| ISBN | : |
Summary of Flutter Experiences as a Guide to the Preliminary Design of Lifting Surfaces on Missiles
| Author | : Dennis J. Martin |
| Publisher | : |
| Total Pages | : 21 |
| Release | : 1958 |
| Genre | : Flutter (Aerodynamics) |
| ISBN | : |
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter investigations that may be of interest in missile design. Several types of flutter of concern in missile studies are briefly described. Crude criteria are presented for two of the most common types of flutter to permit a rapid estimate to be made of the probability of the occurrence of flutter. Many of the details of the flutter problem have been omitted, and only the broader elements have been retained so as to give the designer an overall view of the subject.
Applied Artificial Intelligence 2: Medicine, Biology, Chemistry, Financial, Games, Engineering
| Author | : Nenad Filipović |
| Publisher | : Springer Nature |
| Total Pages | : 257 |
| Release | : |
| Genre | : |
| ISBN | : 3031608402 |
Technical Note - National Advisory Committee for Aeronautics
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1076 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
A Compilation of Research Reports of Physical Research Division, Dynamic Loads Division, Loads Division, 1921 - 1973
| Author | : Gloria R. Champine |
| Publisher | : |
| Total Pages | : 134 |
| Release | : 1977 |
| 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
| 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.
Annual Report of the National Advisory Committee for Aeronautics
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 1516 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
