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
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