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- W2277874818 abstract "This report describes the development of a numerical algorithm for the simulation of the unsteady flow field resulting from flutter in an infinite two-dimensional cascade of — flat plates. The Numerical Method of Lines (NMOL) is used in conjunction with a time-marching integrator for the simulation. V, The numerical model of the flow field is developed using a finite isolated airfoil in a nonconvecting fluid. A performance assessment is made of the numerical integration parameters. Optimum parameters are then used to compute trial solutions for finite isolated and cascaded airfoils in a convecting fluid. Computed airfoil loading curves for incompressible flow are examined in light of Theodorsen's potential solution for an isolated flat plate. The flow is assumed compressible, inviscid and isotropic. A discussion of the numerical modelUftj^f the trailing edge and wake region is included." @default.
- W2277874818 created "2016-06-24" @default.
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- W2277874818 date "1980-01-01" @default.
- W2277874818 modified "2023-09-27" @default.
- W2277874818 title "The simulation of unsteady aerodynamics using the numerical method of lines." @default.
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