Geodesic
Problem solution of aerodynamic design using multiprocessor computers
Matematičeskoe modelirovanie i čislennye metody, no. 5 (2015), pp. 17-30 Cet article a éte moissonné depuis la source Math-Net.Ru

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The article discusses a method for constructing an aircraft geometric shape for computing the parameters of aerogasdynamic flow as well as a method of meshing near the model to simulate the flow within the Navier–Stokes equations in the thin layer approximation. The results of the flow simulation are given. The calculations were performed on a multiprocessor computer system.
Keywords: Mathematical modeling, aircraft model, mesh, Navier–Stokes equation, hypersonic flow. 
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     author = {A. V. Bratchev and A. Yu. Dubrovina and V. P. Kotenev and F. A. Maximov and Yu. D. Shevelev},
     title = {Problem solution of aerodynamic design using multiprocessor computers},
     journal = {Matemati\v{c}eskoe modelirovanie i \v{c}islennye metody},
     pages = {17--30},
     year = {2015},
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     url = {http://geodesic.mathdoc.fr/item/MMCM_2015_5_a1/}
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A. V. Bratchev; A. Yu. Dubrovina; V. P. Kotenev; F. A. Maximov; Yu. D. Shevelev. Problem solution of aerodynamic design using multiprocessor computers. Matematičeskoe modelirovanie i čislennye metody, no. 5 (2015), pp. 17-30. http://geodesic.mathdoc.fr/item/MMCM_2015_5_a1/

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