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• W2313855359 abstract "An integrated computational fluid dynamics and computational structural dynamics (CFD-CSD) approach is being developed for the simulation and prediction of transonic flutter. The CFD solver was based on an unsteady, parallel, multi-block, multi-grid, structured, finite volume algorithm for the Euler/Navier-Stokes equations. The solution of the flowfield is coupled with the structural dynamics by a fully implicit method. The twodimensional (2D) CSD solver is based on the time integration of a two-degree-of-freedom (two-DOF) structural model while the three-dimensional (3D) CSD solver is a finite element model. The coupled CFD-CSD method simulates the elastic system directly in the time domain to determine the stability and response of the aeroelastic system." @default.
• W2313855359 created "2016-06-24" @default.
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• W2313855359 date "2016-01-02" @default.
• W2313855359 modified "2023-09-25" @default.
• W2313855359 title "Methodology Development for Coupled Aeroelastic Analysis of Wing Flutter" @default.
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• W2313855359 doi "https://doi.org/10.2514/6.2016-1550" @default.
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