Gas-dynamic design of an axisymmetric tunnel air inlet with isentropic compression

Bibliographic Details
Parent link:	Journal of Applied Mechanics and Technical Physics.— , 1965- Vol. 56, iss. 5.— 2015.— [P. 831-837]
Main Author:	Galkin V. M. Vladislav Mikhailovich
Corporate Author:	Национальный исследовательский Томский политехнический университет (ТПУ) Институт природных ресурсов (ИПР) Кафедра геологии и разработки нефтяных месторождений (ГРНМ)
Other Authors:	Vnuchkov D. A., Zvegintsev V. I.
Summary:	Title screen A method of designing a supersonic axisymmetric tunnel air inlet based on the problem of an inverted flow in an annular nozzle with isentropic expansion is considered. The nozzle contour is constructed by the method of characteristics. Parameters of one inlet for viscous and inviscid gas flows are calculated. Режим доступа: по договору с организацией-держателем ресурса
Language:	English
Published:	2015
Subjects:	электронный ресурс труды учёных ТПУ
Online Access:	http://dx.doi.org/10.1134/S0021894415050090
Format:	Electronic Book Chapter
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=645703

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