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

Dettagli Bibliografici
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.]
Ente Autore:	Национальный исследовательский Томский политехнический университет Инженерная школа энергетики Научно-образовательный центр И. Н. Бутакова (НОЦ И. Н. Бутакова)
Altri autori:	Maslov E. A. Evgeny Anatolievich, Zharova I. Irina, Faraponov V. Valery, Kozlov E. Eugene, Matskevich V. Vladislav
Riassunto:	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).
Lingua:	inglese
Pubblicazione:	Les Ulis, EDP Sciences, 2018
Soggetti:	электронный ресурс труды учёных ТПУ теплообмен проточные части воздушно-реактивные двигатели газовая динамика потоки газы число Маха
Accesso online:	https://doi.org/10.1051/matecconf/201819401037 http://earchive.tpu.ru/handle/11683/51462
Natura:	Elettronico Capitolo di libro
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=658581

Descrizione
Riassunto:	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).
DOI:	10.1051/matecconf/201819401037

Documenti analoghi