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- W1792508825 abstract "The flow simulation system MEGAFLOW is applied to the Navier-Stokes investigation of the ALVAST wing/fuselage configuration with deployed high-lift system. The comparison of the numerical results to experimental data reveals good agreement and satisfying robustness of the convergence process. The Reynolds-number influence is estimated by increasing the Reynolds-number one order of magnitude, causing essentially an increase of lift on all three components. Within the framework of wake vortex investigations Euler computations have been conducted. For the same angle of attack as well as for the same lift coefficient as used in experiments, the neglect of viscosity yields a deviation from the loading of the single components of the high-lift wing. First evaluations of the wake vortex flowfield behind the configuration yield plausible results." @default.
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- W1792508825 date "1999-01-01" @default.
- W1792508825 modified "2023-09-27" @default.
- W1792508825 title "Numerical Flow Simulation for a Wing/Fuselage Transport Aircraft Configuration with Deployed High-Lift System" @default.
- W1792508825 cites W163008363 @default.
- W1792508825 doi "https://doi.org/10.1007/978-3-663-10901-3_47" @default.
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