Numerical investigation of the interaction of twin supersonic jet with a flat obstacle
This paper presents the results of mathematical modeling of the interaction of supersonic twin jet flow with a flat obstacle. The influence of the distance between the nozzles on the shock-wave structure of the gas flow for the Mach numbers 4.7 on the nozzle exit are studied. In the studies, the dis...
| Published in: | AIP Conference Proceedings Vol. 2351. P. 030062-1-030062-6 |
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| Other Authors: | , , , |
| Format: | Article |
| Language: | English |
| Subjects: | |
| Online Access: | http://vital.lib.tsu.ru/vital/access/manager/Repository/koha:000901899 Перейти в каталог НБ ТГУ |