I want to calculating eigenvalues and eigenvectors by Lnaczos reduction method for using in unsteady aerodynamic field. At first, I simulated cavity flow by using first order implicit method. Incompressible Navier-Stokes and virtual compressibility were used for solving governing equations. Some results of this work were shown.
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Schematic of Grid Generation for Simulation Cavity Flow.
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Path line of Cavity Flow (Re=100).
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Contour of U_Velocity (Re=100).
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Contour of V_Velocity (Re=100).
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