Сибирский федеральный университет

Тип публикации: статья из журнала

Год издания: 2013

Идентификатор DOI: 10.1016/j.proeng.2013.07.086

Ключевые слова: Time-dependent Navier-Stokes equations, heat-conducting gas, four-stage computational technology, high-order solvers

Аннотация: All three components of computational aerodynamics are actively developed: mathematical models of real aerodynamic processes, numerical algorithms, and high-performance computing. The most impressive progress has been made in the field of computing, though with a considerable complication of the computer architecture. Numerical algorithms developed more conservative. Nevertheless, computational mathematics now amassed a whole palette of numerical algorithms that can provide acceptable accuracy and interface between modern mathematical models in aerodynamics and high-performance computers. This paper gives a general overview of objectives and approaches of international Project TRISTAM and a description of the four-stage computer technology in the field of computational aerodynamics.

Журнал: Procedia Engineering

Выпуск журнала: Т. 61

Номера страниц: 16-22

ISSN журнала: 18777058

Издатель: Elsevier BV

• Shaydurov V. (Institute of Computational Modelling, Siberian Branch of the Russian Academy of Sciences)
• Liu T.

• РИНЦ (eLIBRARY.RU)