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Simulation of Flow around Wing Sections by Building-Cube Method

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Abstract

Flow around an airplane includes various scales; from micro-scale near the surface to macro-scale around the airplane. The macro-scale flow basically determines the surface pressure distribution around an airplane. The microscale flow dynamics also has a significant contribution to such as the skin friction, the flow separations and the aerodynamic noise generation. Current CFD has become a powerful tool to accurately simulate macro-scale flows for designing airplanes. The micro-scale flow simulation, however, is still difficult due to the extremely large difference in the flow characteristic length.

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References

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Correspondence to Kazuhiro Nakahashi .

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© 2009 Springer-Verlag Berlin Heidelberg

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Nakahashi, K., Sakurai, Y. (2009). Simulation of Flow around Wing Sections by Building-Cube Method. In: Deconinck, H., Dick, E. (eds) Computational Fluid Dynamics 2006. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-92779-2_61

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  • DOI: https://doi.org/10.1007/978-3-540-92779-2_61

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-92778-5

  • Online ISBN: 978-3-540-92779-2

  • eBook Packages: EngineeringEngineering (R0)

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