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- W2767046865 abstract "Coaxial jets originating from a nozzle interacting with a two-element wing configuration consisting of a main wing and a flap are computed using large-eddy simulations (LES) to investigate in the long term the effect of the interaction on the sound field of this jet-wing-flap configuration. The secondary jet Mach number is (M_s=0.37) and the Reynolds number based on the secondary velocity and diameter is (Re_{s}=1.32 times 10^6). The nozzle inlet boundary layers are modeled by Blasius velocity profiles with a boundary layer thicknesses of 20% of the nozzle channel half-width. The acoustic far-field is predicted by solving the linearized Euler equations (LEE) in a region attached to the LES domain. The jet streams interacts with the two-element wing configuration and lead to a significantly changed mean flow field in the wing-flap gap area and pressure at the wing surface. Additionally, a strong influence of the flap on the jet development is observed, especially in the case of a non-zero free stream velocity." @default.
- W2767046865 created "2017-11-10" @default.
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- W2767046865 date "2017-10-31" @default.
- W2767046865 modified "2023-09-27" @default.
- W2767046865 title "Towards the Prediction of Flow and Acoustic Fields of a Jet-Wing-Flap Configuration" @default.
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- W2767046865 doi "https://doi.org/10.1007/978-3-319-64519-3_59" @default.
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