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Matematicheskoe Modelirovanie i Chislennye Metody, 2015, Issue 5, Pages 17–30
(Mi mmcm33)
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Problem solution of aerodynamic design using multiprocessor computers
A. V. Bratcheva, A. Yu. Dubrovinaa, V. P. Kotenevba, F. A. Maximovc, Yu. D. Shevelevc a JSC "MIC "NPO Mashinostroyenia"
b Bauman Moscow State Technical University
c Institute for Computer Aided Design of RAS, Moscow
Abstract:
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.
Received: 07.04.2015
Citation:
A. V. Bratchev, A. Yu. Dubrovina, V. P. Kotenev, F. A. Maximov, Yu. D. Shevelev, “Problem solution of aerodynamic design using multiprocessor computers”, Mat. Mod. Chisl. Met., 2015, no. 5, 17–30
Linking options:
https://www.mathnet.ru/eng/mmcm33 https://www.mathnet.ru/eng/mmcm/y2015/i5/p17
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