Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels

Numerical design of multimodal axisymmetric hypersonic nozzles for wind tunnels

Bibliographic Details
Parent link:Journal of Applied Mechanics and Technical Physics: Scientific Journal
Vol. 51, iss. 2.— 2010.— [P. 218-225]
Corporate Author: Национальный исследовательский Томский политехнический университет (ТПУ)
Other Authors: Aulchenko S. M., Galkin V. M. Vladislav Mikhailovich, Zvegintsev V. I., Shiplyuk A. N.
Summary: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
Language:English
Published: 2010
Subjects:
электронный ресурс
труды учёных ТПУ
Online Access:http://dx.doi.org/10.1007/s10808-010-0031-0
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=636478

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