Computer Aided Derivation of Linearized Dynamical Models for Stability Analysis. Part 2. Sample Model. A Wind Turbine Rotor.

摘要

The report accompanies The computer aided derivation of linearized dynamical models for stability analysis; part I: Description of the general model, which deals with the more general description of the applied method. In that report some theoretical background is given. The report is written in order to illustrate the described procedure in the previous report. A linearized stability model is derived for a simple wind turbine rotor flap-lag configuration, similar to the one previously used by Chopra & Dugundji. The procedure is followed step by step and the generated output of each step is included in the appendices.