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Published in 2017 at "CEAS Aeronautical Journal"
DOI: 10.1007/s13272-017-0243-6
Abstract: In the present work, a reduced order model (ROM) for aeroelastic analysis linearized around non-linear steady solutions has been assessed and implemented to perform high-fidelity predictions, in particular for transonic flow. The ROM has been…
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Keywords:
rom linearized;
development rom;
aeroelastic analysis;
rom ... See more keywords