Study of heat transfer processes in the flowing part of hypersonic air-ramjet engine

Study of heat transfer processes in the flowing part of hypersonic air-ramjet engine

Bibliographic Details
Parent link:MATEC Web of Conferences
Vol. 194 : Heat and Mass Transfer in the Thermal Control System of Technical and Technological Energy Equipment (HMTTSC 2018).— 2018.— [01037, 5 p.]
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, Zharova I. Irina, Faraponov V. Valery, Kozlov E. Eugene, Matskevich V. Vladislav
Summary:Title screen
The technique and results of the experimental-theoretical study of gas dynamics, heat transfer and the structure of gas flow in the flowing channel of a model hypersonic air-ramjet engine are presented for Mach numbers M (5; 6).
Language:English
Published: Les Ulis, EDP Sciences, 2018
Subjects:
электронный ресурс
труды учёных ТПУ
теплообмен
проточные части
воздушно-реактивные двигатели
газовая динамика
потоки
газы
число Маха
Online Access:https://doi.org/10.1051/matecconf/201819401037
http://earchive.tpu.ru/handle/11683/51462
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=658581

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