MATEC Web of Conferences

MATEC Web of Conferences

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).

Bibliographic Details
Other Authors: Maslov specialist in the field of power engineering Associate Professor of Tomsk Polytechnic University, Candidate of physical and mathematical sciences, Zharova, Faraponov, Kozlov, Matskevich
Format: Book Chapter
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

Internet

https://doi.org/10.1051/matecconf/201819401037
http://earchive.tpu.ru/handle/11683/51462

Similar Items