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Validation of an unstructured Euler code for the simulation of transonic flows past a complete aircraft

  • Unstructured and Adaptive Grids
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Thirteenth International Conference on Numerical Methods in Fluid Dynamics

Part of the book series: Lecture Notes in Physics ((LNP,volume 414))

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Abstract

A numerical procedure to solve inviscid compressible flows about complex geometries has been described. Numerical solutions of transonic flows around a complete fighter aircraft has been compared with available experimental data. The results are quite satisfactory except in regions where viscous effects are important, which is a known limitation of the numerical model. Overall time for grid generation and solution are sufficiently low to use these tools for production.

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References

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M. Napolitano F. Sabetta

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© 1993 Springer-Verlag

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Hettena, E., Formaggia, L., Antonellini, A., Selmin, V. (1993). Validation of an unstructured Euler code for the simulation of transonic flows past a complete aircraft. In: Napolitano, M., Sabetta, F. (eds) Thirteenth International Conference on Numerical Methods in Fluid Dynamics. Lecture Notes in Physics, vol 414. Springer, Berlin, Heidelberg. https://doi.org/10.1007/3-540-56394-6_227

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  • DOI: https://doi.org/10.1007/3-540-56394-6_227

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-56394-5

  • Online ISBN: 978-3-540-47551-4

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