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- W2019908032 abstract "Airfoil/jet/ground-interaction flowfields are calculated by solving Euler equations on body-conforming curvilinear grids. For these computations, Jameson's Euler code (FLO-53) based on an explicit Runge-Kutta timemarching finite-volume procedure is modified. Euler equations are preconditioned for computing almost incompressible flows. Euler equations capture the vortex formation behind the jet and most of the airfoil/jet/groundplane interaction, except the effect of entrainment. Reasonable agreement is obtained between the calculated and experimental values of the lift on the airfoil for moderate values of jet-velocity to freestream-velocity ratio." @default.
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- W2019908032 date "1986-05-01" @default.
- W2019908032 modified "2023-09-25" @default.
- W2019908032 title "Euler solutions for airfoil/jet/ground-interaction flowfields" @default.
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- W2019908032 doi "https://doi.org/10.2514/3.45318" @default.
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