Investigation of annular supersonic inlets with isentropic compression

Investigation of annular supersonic inlets with isentropic compression

Bibliographic Details
Parent link:Thermophysics and Aeromechanics.— , 1994-
Vol. 23, iss. 5.— 2016.— [P. 645–655]
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: Zvegintsev V. I., Vnuchkov D. A.
Summary: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
Published: 2016
Subjects:
электронный ресурс
труды учёных ТПУ
сопло
сверхзвуковые потоки
идеальный газ
обратный поток
вязкий поток
Online Access:http://dx.doi.org/10.1134/S0869864316050036
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=652985

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