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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

Description
Summary:	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).
Item Description:	Title screen
Bibliography:	[References: 7 tit.]
DOI:	10.1051/matecconf/201819401037