Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels; Journal of Applied Mechanics and Technical Physics; Vol. 51, iss. 2

Dades bibliogràfiques
Parent link:Journal of Applied Mechanics and Technical Physics: Scientific Journal
Vol. 51, iss. 2.— 2010.— [P. 218-225]
Autor corporatiu: Национальный исследовательский Томский политехнический университет (ТПУ)
Altres autors: Aulchenko S. M., Galkin V. M. Vladislav Mikhailovich, Zvegintsev V. I., Shiplyuk A. N.
Sumari: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
Idioma:anglès
Publicat: 2010
Matèries:
Accés en línia:http://dx.doi.org/10.1007/s10808-010-0031-0
Format: Electrònic Capítol de llibre
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=636478

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