Numerical analysis of geometrical nonlinear aeroelasticity with CFD/CSD method
نویسندگان
چکیده
Abstract A nonlinear static aeroelastic methodology based on the coupled CFD/CSD approach has been developed to study geometrical behaviors of high-aspect-ratio or multi-material flexible aerial vehicles under aerodynamic loads. The Reynolds-averaged Navier–Stokes solver combined with three-dimensional finite-element is used perform fluid-structure coupling simulation. interpolation technique for data transfer between and structural modules employs radial basis function algorithm as well dynamic mesh deformation. structure modeled by finite element method investigate effects nonlinearity behavior. Numerical simulations linear aeroelasticity were conducted at transonic regime different angles attack. By comparing structure, it shows that plays an important role wings undergoing large deformation should be taken into account in analysis such structures.
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ژورنال
عنوان ژورنال: International Journal of Nonlinear Sciences and Numerical Simulation
سال: 2021
ISSN: ['1565-1339', '2191-0294']
DOI: https://doi.org/10.1515/ijnsns-2015-0096