The problem of helicopter mechanical instability is considered for the case where one blade damper is inoperative. It is shown that, if the hub is considered to be nonisotropic, the equations of motion have periodic coefficients which cannot be eliminated. However, if the hub is isotropic, the equations can be transformed to a rotating frame of reference and the periodic coefficients 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.
An application of Floquet theory to prediction of mechanical instability
Specialists Meeting on Rotorcraft Dynamics ; 1974 ; Moffett Field, CA
1974-01-01
Miscellaneous
No indication
English
An application of Floquet theory to prediction of mechanical instability
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