Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods

Design of multimode axisymmetric hypersonic nozzles with the use of optimization methods

Bibliographic Details
Parent link:	Journal of Engineering Physics and Thermophysics: Scientific Journal Vol. 82, iss. 6.— 2009.— [P. 1127-1131]
Corporate Author:	Томский политехнический университет (ТПУ)
Other Authors:	Aulchenko S. M., Galkin V. M. Vladislav Mikhailovich, Zvegintsev V. I., Shiplyuk A. N.
Summary:	Title screen On the basis of the solution of direct problems with the use of various medium models and numerical methods of integration of gas flow equations, methods for designing super- and hypersonic nozzles have been developed. Multimode nozzles in the ranges of Mach numbers 8-14 and 14-20 satisfying given conditions have been designed. Режим доступа: по договору с организацией-держателем ресурса
Published:	2009
Subjects:	электронный ресурс труды учёных ТПУ
Online Access:	http://dx.doi.org/10.1007/s10891-010-0306-6
Format:	Electronic Book Chapter
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=636476

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