IDENTIFICATION OF STRUCTURAL DAMPING OF A HELICOPTER ROTOR BLADE

Authors

  • T. Gausz

Abstract

In the elastic motion of helicopter rotor blades the structural damping also has an important role, The purpose of this article is the investigation of the mathematical model of the structural damping and the estimation of the parameters of this model. The parameter estimation is based on measurings (the first three natural oscillations were measured).

Keywords:

structural damping, identification, rotor blade.

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How to Cite

Gausz, T. (1993) “IDENTIFICATION OF STRUCTURAL DAMPING OF A HELICOPTER ROTOR BLADE ”, Periodica Polytechnica Transportation Engineering, 21(4), pp. 299–302.

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Section

Articles