Investigation of annular supersonic inlets with isentropic compression; Thermophysics and Aeromechanics; Vol. 23, iss. 5

Investigation of annular supersonic inlets with isentropic compression; Thermophysics and Aeromechanics; Vol. 23, iss. 5

Podrobná bibliografie
Parent link:Thermophysics and Aeromechanics.— , 1994-
Vol. 23, iss. 5.— 2016.— [P. 645–655]
Hlavní autor: Galkin V. M. Vladislav Mikhailovich
Korporativní autor: Национальный исследовательский Томский политехнический университет (ТПУ) Институт природных ресурсов (ИПР) Кафедра геологии и разработки нефтяных месторождений (ГРНМ)
Další autoři: Zvegintsev V. I., Vnuchkov D. A.
Shrnutí:Title screen
A technique for designing the supersonic annular inlets with isentropic deceleration surfaces is considered. The contour of an isentropic supersonic nozzle constructed by the method of characteristics for an inviscid gas flow with given uniform parameters at the inlet and at the outlet is used as the basic configuration of the inlet. The reversed flow of a viscous gas is computed with the aid of numerical techniques in the contour under consideration and the real operational characteristics of the obtained inlet of a fixed geometry are determined in the range of the conditions of its application. In the process of computations, the minimum cross-sectional sizes are selected, which ensure the inlet start without a detached bow shock at the entrance.
Режим доступа: по договору с организацией-держателем ресурса
Jazyk:angličtina
Vydáno: 2016
Témata:
электронный ресурс
труды учёных ТПУ
сопло
сверхзвуковые потоки
идеальный газ
обратный поток
вязкий поток
On-line přístup:http://dx.doi.org/10.1134/S0869864316050036
Médium: Elektronický zdroj Kapitola
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=652985

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