Summary
A set of 3D Navier-Stokes solutions around a complete wing-body-tail configuration is presented for different mesh resolutions. The local mesh dependent behaviour is investigated and from these experiences, a technique is derived that aims for multi-sweep y+ driven mesh adaptation to wing- and fuselage boundary layer profiles. This technique is described and demonstrated but final results are still under preparation.
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E. Coustols, A. Seraudie, A. Mignosi: Rear-Fuselage Transonic Flow Characteristics for a Complete Wing-Body Configuration. J. Aircraft, Vol.34, No.3, pp.337-345.
E. Elholz, H. Steinmeyer: Mesh Modification Techniques for Navier-Stokes Meshes. Demonstration of Viscous Adaptation, Geometry Change and Mesh Enrichment. In: H.Körner, R. Hilbig (Eds): New Results in Numerical and Experimental Fluid Mechanics. Notes on Numerical Fluid Mechanics, Vol.60, Vieweg 1997.
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© 1999 Springer Fachmedien Wiesbaden
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Elsholz, E., Steinmeyer, H., John, D. (1999). Navier-Stokes Solutions on Wing-Body-Tail Configurations and Viscous Mesh Adaptation Technique. In: Nitsche, W., Heinemann, HJ., Hilbig, R. (eds) New Results in Numerical and Experimental Fluid Mechanics II. Notes on Numerical Fluid Mechanics (NNFM), vol 72. Vieweg+Teubner Verlag, Wiesbaden. https://doi.org/10.1007/978-3-663-10901-3_16
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DOI: https://doi.org/10.1007/978-3-663-10901-3_16
Publisher Name: Vieweg+Teubner Verlag, Wiesbaden
Print ISBN: 978-3-663-10903-7
Online ISBN: 978-3-663-10901-3
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