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- W2016207724 abstract "Unsteady inviscid transonic airfoil-vortex interaction is numerically analyzed by solving the two-dimensional unsteady Euler equations in integral form using a finite volume scheme. The solution procedure is based on an explicit Runge-Kutta time-stepping scheme wherein the spatial terms are central-differenced and a combination of second- and fourth-differences in the flow variables is used to form the numerical dissipation terms to stabilize the scheme. A velocity decomposition technique is applied to alleviate the problem of vortex diffusion by the numerical dissipation terms and to treat the interaction of a Rankine vortex with an airfoil accurately. Results obtained are compared with available numerical data." @default.
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- W2016207724 date "1987-06-08" @default.
- W2016207724 modified "2023-10-16" @default.
- W2016207724 title "A finite volume Euler calculation of the aerodynamics of transonic airfoil-vortex interaction" @default.
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- W2016207724 doi "https://doi.org/10.2514/6.1987-1244" @default.
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