This article is cited in 19 papers

Development of mathematical models and numerical methods for aerodynamic design on multiprocessor computers

F. A. Maximov, D. A. Churakov, Yu. D. Shevelev

Institute for Computer-Aided Design, Russian Academy of Sciences, Vtoraya Brestskaya ul. 19/18, Moscow, 123056 Russia

Abstract: Complex-geometry design and grid generation are addressed. The gasdynamic equations are solved, and the numerical results are compared with experimental data. For aerodynamic problems, a suite of mathematical and information technology tools is proposed for the support and management of geometric models of actual objects. Based on the mathematical modeling methods developed, numerical experiments can be performed for a wide class of geometric forms and the aerodynamic properties of aircraft can be predicted with allowance for the viscosity effects.

Key words: Navier–Stokes equations, design of aerodynamic forms, flow separation, vortex structures, numerical experiment.

UDC: 519.64

Received: 06.09.2010

 English version: Computational Mathematics and Mathematical Physics, 2011, 51:2, 284–307

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