Abstract
This chapter describes the common effort of UMIST, EADS-CASA, ALENIA and TUB to compute the steady vortex evolving at the round tip of a wing at 10° angle of attack. Results for different numerical grids obtained by the aforementioned four partners using a variety of codes and turbulence models are presented in comparison to experimental data. The main parameters of influence and suggestions for future computations of that case are identified.
and partners ALENIA, EADS-CASA, UMIST
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© 2006 Springer-Verlag Berlin Heidelberg
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Albrecht, P., Wu, D., Martin, A., Bunge, U., Thiele, F. (2006). NACA0012 wing with rounded tip. In: Haase, W., Aupoix, B., Bunge, U., Schwamborn, D. (eds) FLOMANIA — A European Initiative on Flow Physics Modelling. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 94. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-39507-2_25
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DOI: https://doi.org/10.1007/978-3-540-39507-2_25
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-28786-5
Online ISBN: 978-3-540-39507-2
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