Development of mathematical models and numerical methods for aerodynamic design on multiprocessor computers
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 51 (2011) no. 2, pp. 303-328
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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.
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F. A. Maximov; D. A. Churakov; Yu. D. Shevelev. Development of mathematical models and numerical methods for aerodynamic design on multiprocessor computers. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 51 (2011) no. 2, pp. 303-328. http://geodesic.mathdoc.fr/item/ZVMMF_2011_51_2_a8/

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