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Simulation of flow over the ONERA M6 wing using a parallel implementation of an implicit scheme

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Abstract

The flow over the ONERA M6 wing is numerically simulated using a parallel implementation of an implicit scheme with a third-order spatial approximation for the three-dimensional Reynoldsaveraged Navier-Stokes equations based on the Spalart-Allmaras turbulence model modified by Edwards. The scalability of this parallel implementation is studied. The numerical results obtained are compared with experimental data and with the results obtained using an explicit scheme.

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Authors and Affiliations

  1. Faculty of Mechanics and Mathematics, Leninskie Gory, Moscow State University, Moscow, 119899, Russia

    V. E. Borisov

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  1. V. E. Borisov
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Correspondence to V. E. Borisov.

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Original Russian Text © V.E. Borisov, 2015, published in Vestnik Moskovskogo Universiteta, Matematika. Mekhanika, 2015, Vol. 70, No. 4, pp, 65-68.

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Borisov, V.E. Simulation of flow over the ONERA M6 wing using a parallel implementation of an implicit scheme. Moscow Univ. Mech. Bull. 70, 97–100 (2015). https://doi.org/10.3103/S0027133015040044

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  • DOI: https://doi.org/10.3103/S0027133015040044

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