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Nonlinear dynamic response of wind turbine rotors. Ph. D. thesis - MIT

Technical Report ·
OSTI ID:6239977
The nonlinear equations of motion for a rigid rotor restrained by three flexible springs representing the flapping, lagging and feathering motions are derived using Lagrange's equations for arbitrary angular rotations. These are reduced to a consistent set of nonlinear equations using nonlinear terms up to third order.
Research Organization:
National Aeronautics and Space Administration, Moffett Field, CA (USA). Ames Research Center
OSTI ID:
6239977
Report Number(s):
N-79-12542
Country of Publication:
United States
Language:
English