Influence of the local gas injection on the flow structure in the boundary layer

Dettagli Bibliografici
Parent link:	MATEC Web of Conferences Vol. 110 : Heat and Mass Transfer in the Thermal Control System of Technical and Technological Energy Equipment (HMTTSC 2017).— 2017.— [01055, 5 p.]
Ente Autore:	Национальный исследовательский Томский политехнический университет (ТПУ) Энергетический институт (ЭНИН) Кафедра атомных и тепловых электростанций (АТЭС)
Altri autori:	Maslov E. A. Evgeny Anatolievich, Savkina N. Nadezhda, Zharova I. Irina, Faraponov V. Valery, Kozlov E. Evgeny, Matskevich V. Vladislav
Riassunto:	Title screen The results of an experimental and numerical study of the interaction of supersonic flow around an axisymmetric model, M = (2 [-:] 5), with a jet of gas injected locally into the boundary layer are presented.
Pubblicazione:	2017
Soggetti:	электронный ресурс труды учёных ТПУ газы течение пограничные слои экспериментальные исследования численные исследования сверхзвуковое обтекание
Accesso online:	https://doi.org/10.1051/matecconf/201711001055 http://earchive.tpu.ru/handle/11683/42620
Natura:	Elettronico Capitolo di libro
KOHA link:	https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=655369

Descrizione
Riassunto:	Title screen The results of an experimental and numerical study of the interaction of supersonic flow around an axisymmetric model, M = (2 [-:] 5), with a jet of gas injected locally into the boundary layer are presented.
DOI:	10.1051/matecconf/201711001055

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