A multi-fidelity framework for physics based rotor blade simulation and optimization
New helicopter rotor designs are desired that offer increased efficiency, reduced vibration, and reduced noise. This problem is multidisciplinary, requiring knowledge of structural dynamics, aerodynamics, and aeroacoustics. Rotor optimization requires achieving multiple, often conflicting objectives...
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Georgia Institute of Technology
2009
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| Online Access: | http://hdl.handle.net/1853/26481 |