Summary
The flow field and the acoustic field of a high-lift configuration consisting of a slat and a main wing are numerically investigated by an efficient hybrid LES/CAA method. The flow parameters are Ma = 0.16, Re = 1.4*106, and α= 13 deg. The simulated flow is in good agreement with experimental findings. The turbulent flow structures especially in the slat cove shear layer reveal patterns similar to those observed in a plane shear layer and an impinging jet, respectively. The acoustic analyses identify the slat gap as the origin of tonal and broadband noise ranging from 1 to 3 kHz.
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König, D. et al. (2010). Analysis of High-Lift Generated Noise via a Hybrid LES/CAA Method. In: Dillmann, A., Heller, G., Klaas, M., Kreplin, HP., Nitsche, W., Schröder, W. (eds) New Results in Numerical and Experimental Fluid Mechanics VII. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 112. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-14243-7_55
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DOI: https://doi.org/10.1007/978-3-642-14243-7_55
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