Инд. авторы:	Semionov N.V., Yermolaev Y.G., Kosinov A.D., Dryasov A.D., Semenov A.N., Yatskikh A.A.
Заглавие:	The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing
Библ. ссылка:	Semionov N.V., Yermolaev Y.G., Kosinov A.D., Dryasov A.D., Semenov A.N., Yatskikh A.A. The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing // Fourth International Symposium on Negative Ions, Beams and Sources (NIBS 2014). - 2016. - Vol.1770. - Art.030050. - ISBN 978-0-7354-1297-2. - ISSN 0094-243X.
Внешние системы:	DOI: 10.1063/1.4963992; SCOPUS: 2-s2.0-84994083549;
Реферат:	eng: The paper is devoted to an experimental study of laminar-turbulent transition in a three-dimensional supersonic boundary layer. The experiments were conducted at the low nose supersonic wind tunnel T-325 of ITAM at Mach numbers M=2 - 4. Model is a symmetrical wing with a 45° sweep angle, a 3 percent-thick circular-arc airfoil. The influence of flow parameters, such as the Mach number, unit Reynolds number, angle of attack, level of perturbations on the transitions to turbulence are on the consideration. Transition Reynolds numbers are obtained. Analysis of all obtained data allow to determine reliable value of Retr of swept wing supersonic boundary layer, that especially important at consideration of experiments fulfilled at different flow conditions in different wind tunnels. © 2016 Author(s).
Издано:	2016
Физ. характеристика:	030050
Конференция:	Название: 4th International Symposium on Negative Ions, Beams and Sources Аббревиатура: NIBS-2014 Город: Garching Страна: Germany Даты проведения: 2014-10-06 - 2014-10-10