Christian T. Nitschke, Jonas Maruani, Angela Vincenti, Didier Lucor, Jean-Camille Chassaing

DOI Number: N/A

Conference number: IFASD-2015-182

The aeroelastic response of a cantilevered composite plate wing in incompressible flow is studied. Uncertainties of the laminate ply angles are taken into account, with special regard to desymmetrisation of the laminate by the uncertainties. The polar method is employed for preliminary analysis as well as parameter space reduction. Arbitrary polynomial chaos is used to decrease the number of calls to the aeroelastic solver.

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In Categories: 2. IFASD 2015, Nonlinearities & Uncertainties
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