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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Selmin L., Hettena E., Formaggia L.: “An Unstructured Node Centered Scheme for the Simulation of 3-D Inviscid Flows”, in Proceedings of the First European Computational Fluid Dynamic conference (1992).
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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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