The problem of helicopter mechanical instability is considered for the case where one blade damper is inoperative, and it is shown that if the hub is considered to be nonisotropic, the equations of motion have periodic coefficients which cannot be eliminated. The Floquet transition matrix method is shown to be an effective way of dealing with the nonisotropic hub and nonisotropic rotor situation. Time history calculations are examined and shown to be inferior to the Floquet technique for determining system stability. It is shown that instabilities which occur when one blade damper is inoperative may consist of nearly pure blade motion or they may be similar to the classical mechanical instability.
An application of Floquet theory to prediction of mechanical instability
1974-01-01
Conference paper
No indication
English
An application of Floquet theory to prediction of mechanical instability
Tema Archive | 1974
|Floquet Instability in Periodically Reversing Flows
British Library Conference Proceedings | 2023
|Fast Floquet Theory and Trim for Multi-Bladed Rotorcraft
British Library Conference Proceedings | 1995
|