Investigation of working processes in a flowing channel of ramjet engine

Investigation of working processes in a flowing channel of ramjet engine

Bibliographic Details
Parent link:Thermal Science
Vol. 23.— 2019.— [P. 531-536]
Corporate Author: Национальный исследовательский Томский политехнический университет Инженерная школа энергетики Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)
Other Authors: Maslov E. A. Evgeny Anatolievich, Faraponov V. V., Arkhipov V. A. Vladimir Afanasjevich, Zharova I. K. Irina Konstantinovna, Kozlov E. A. Evgeny Aleksandrovich, Savkina N. V. Nadezhda Valerjevna
Summary:Title screen
The technique and results of experimental-theoretical study of gas-dynamics, heat transfer and the structure of gas-flow in the flowing channel of a ramjet engine in Mach number range M = (5-7) are presented. The temperature distribution along the flowing channel of a ramjet engine was experimentally obtained. The temperature along the wall of the flowing channel of the axisymmetric model was measured using the developed thermo-probe. Distributions of Mach number and temperature along the symmetry axis of the flowing channel of the model are obtained numerically. Comparison of the numerical and experimentally obtained values of the Mach number showed their qualitative agreement.
Language:English
Published: 2019
Subjects:
электронный ресурс
труды учёных ТПУ
gas dynamics
heat transfer
supersonic flow
experimental research
mathematical modeling
газовая динамика
теплообмен
сверхзвуковые потоки
экспериментальные исследования
математическое моделирование
Online Access:https://doi.org/10.2298/TSCI19S2531M
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=660412

Internet

https://doi.org/10.2298/TSCI19S2531M

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