Документ взят из кэша поисковой машины. Адрес оригинального документа : http://num-meth.srcc.msu.ru/english/zhurnal/tom_2010/v11r201.html
Дата изменения: Wed Jan 27 14:13:45 2010
Дата индексирования: Mon Oct 1 22:46:03 2012
Кодировка:
"Remote computer simulation of shock-wave structures in hypersonic gas flows: "workplace as a service" cloud computing technology"  
"Remote computer simulation of shock-wave structures in hypersonic gas flows: "workplace as a service" cloud computing technology"
Tarnavsky G.A.

Computer tools for mathematical simulation of shock-wave structures in real gas high-speed flow at the inlet to a diffuser of a hypersonic scramjet engine are considered. Computational process is organized using the "Software, Infrastructure and Workplace as a Service" Cloud Computing technologies.

Keywords: real gas, shock waves, hypersonic streams, information technologies, computer simulation, cloud computing

Tarnavsky G.A.   e-mail: vabishchevich@gmail.com