Hitoshi Arizono, Hamid Reza Kheirandish

DOI Number: N/A

Conference number: IFASD-2019-011

This paper describes that a new aeroelastic simulation code based on the unstructured CFD solver is developed. Computations are performed for AGARD 445.6 wing model and BSCW wing model. The Flutter boundary predicted by the developed code are presented and compared with the experimental data.

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In Categories: IFASD 2019, Unsteady CFD
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