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- W2023688574 abstract "Unsteady inviscid transonic flow over airfoils in arbitrary rigid body motion is analyzed numerically 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 are used to form the numerical dissipation terms to stabilize the scheme. Unsteady calculations are started from converged steady-state solutions as initial conditions. Nonreflective boundary conditions are imposed on the far-field boundaries. Results are presented and, where possible, validated against available numerical and experimental data for airfoils subjected to a step change in angle of attack, airfoils oscillating and plunging in transonic flow, and airfoils immersed in a time-varying free stream." @default.
- W2023688574 created "2016-06-24" @default.
- W2023688574 creator A5059448435 @default.
- W2023688574 date "1988-01-11" @default.
- W2023688574 modified "2023-09-22" @default.
- W2023688574 title "Finite volume computation of unsteady inviscid rotational transonic flows past airfoils in rigid body motion" @default.
- W2023688574 cites W2072287851 @default.
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- W2023688574 doi "https://doi.org/10.2514/6.1988-6" @default.
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