Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels; Journal of Applied Mechanics and Technical Physics; Vol. 51, iss. 2
| Parent link: | Journal of Applied Mechanics and Technical Physics: Scientific Journal Vol. 51, iss. 2.— 2010.— [P. 218-225] |
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| Ente Autore: | |
| Altri autori: | , , , |
| Riassunto: | Title screen A method for design of hypersonic nozzles for wind tunnels is developed and implemented on the basis of solving direct problems with various models of the medium and numerical methods of integration of gas-flow equations. Multimodal nozzles for operation in Mach number ranges Mout = 8-14 and Mout = 14-20 satisfying specified requirements are designed. Режим доступа: по договору с организацией-держателем ресурса |
| Lingua: | inglese |
| Pubblicazione: |
2010
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| Soggetti: | |
| Accesso online: | http://dx.doi.org/10.1007/s10808-010-0031-0 |
| Natura: | Elettronico Capitolo di libro |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=636478 |