Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels

Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels

Podrobná bibliografie
Parent link:Journal of Applied Mechanics and Technical Physics: Scientific Journal
Vol. 51, iss. 2.— 2010.— [P. 218-225]
Korporativní autor: Национальный исследовательский Томский политехнический университет (ТПУ)
Další autoři: Aulchenko S. M., Galkin V. M. Vladislav Mikhailovich, Zvegintsev V. I., Shiplyuk A. N.
Shrnutí: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
Vydáno: 2010
Témata:
электронный ресурс
труды учёных ТПУ
On-line přístup:http://dx.doi.org/10.1007/s10808-010-0031-0
Médium: Elektronický zdroj Kapitola
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=636478

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