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- W2016454716 abstract "The work is devoted to 3D and 2D parallel numerical computation of pressure and velocity fields around an elastically supported airfoil self-oscillating due to interaction with the airflow. Numerical solution is computed in the OpenFOAM package, an open-source software package based on finite volume method. Movement of airfoil is described by translation and rotation, identified from experimental data. A new boundary condition for the 2DOF motion of the airfoil was implemented. The results of numerical simulations (velocity) are compared with data measured in a wind tunnel, where a physical model of NACA0015 airfoil was mounted and tuned to exhibit the flutter instability. The experimental results were obtained previously in the Institute of Thermomechanics by interferographic measurements in a subsonic wind tunnel in Nový Knín." @default.
- W2016454716 created "2016-06-24" @default.
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- W2016454716 date "2014-01-01" @default.
- W2016454716 modified "2023-09-27" @default.
- W2016454716 title "Parallel numerical simulation of oscillating airfoil NACA0015 in the channel due to flutter instability" @default.
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- W2016454716 doi "https://doi.org/10.1051/epjconf/20146702098" @default.
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