Abstract
Maximum lift prediction for a modern realistic transport high-lift configurations using a Computational Fluid Dynamics (CFD) based method still poses a significant challenge. The flow around a high-lift aircraft configuration can be characterized by a number of physical flow features such as flow separation, laminar/ turbulent boundary layers, wakes of wing elements, vortical flows structures, vortex break down, but also deformation of the wing and its components. The accurate modelling of these individual physical features require the development, verification and validation of specific CFD algorithms. This paper focuses only on one of these algorithms, namely a time-integration algorithm.
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References
Eliasson, P., Marongiu, C., Mikhaylov, S., Vlasenko, V., Bosnyakov, S., Kazhan, E.: Acceleration of URANS for application to separated high-lift flows. In: Eberhardsteiner, J., et al. (eds.) European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2012), Vienna, Austria, September 10-14 (2012)
Acisu, I.: Maximum lift computations using unsteady RANS with a Reynolds Stress Model. Presented at the ComFlite final Workshop (June 2012)
Knobloch, O.: Untersuchung der Fahigkeiten von URANS, verbesserte ablösenahe und abgelöste Strömungen im Bereich des Maximalauftriebs vorherzusagen, milestone report 2.1.3 (November 2010)
Schwamborn, D., Gerhold, T., Heinrich, R.: The DLR Tau-Code: Recent Applications in Research and Industry. In: Wesseling, P., Oñate, E., Périaux, J. (eds.) Proceedings of the European Conference on Computational Fluid Dynamics ECCOMAS CDF 2006, The Netherlands (2006)
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van der Burg, J.W., Luehmann, M. (2013). Simulation of Maximum Lift Using URANS for a High-Lift Transport Configuration. In: Kroll, N., Radespiel, R., Burg, J., Sørensen, K. (eds) Computational Flight Testing. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 123. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38877-4_6
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DOI: https://doi.org/10.1007/978-3-642-38877-4_6
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-38876-7
Online ISBN: 978-3-642-38877-4
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