Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Semionov Nikolay"'
Publikováno v:
EPJ Web of Conferences, Vol 196, p 00018 (2019)
The experimental study of the effect of weak shock waves on the supersonic boundary layer of the flat plate with a blunt leading edge (the radius of bluntness was r = 2.5 mm) with Mach number M = 2.5 and zero angle of attack was carried out. The meas
Externí odkaz:
https://doaj.org/article/74af482a708141c69017a63630119265
Publikováno v:
MATEC Web of Conferences, Vol 115, p 02015 (2017)
The evolution of the artificial wave packet in swept-wing supersonic boundary layer was experimentally studied at M = 2. The localized disturbances were generated by a pulse glow discharge. Measurements were provided by a hot-wire anemometer. The spa
Externí odkaz:
https://doaj.org/article/3c2f642a863c4621ab5c8dc6212bf2f7
Publikováno v:
In Procedia IUTAM 2015 14:48-57
The work is devoted to the experimental study of the regularities of laminar-turbulent transition in supersonic boundary layers at Mach number M = 2 and 2.5 in the low-noise supersonic wind tunnel T325 of ITAM SB RAS. The measurements were made by a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3bba84cdd38ce5302b65d9f4439c09cf
Autor:
Markovich, D.M., Kuibin, P.A., Vorobyev, M.A., Kocharin, Vasiliy, Kosinov, Aleksandr, Yermolayev, Yuriy, Semionov, Nikolay
Publikováno v:
EPJ Web of Conferences; 2019, Vol. 196, pN.PAG-N.PAG, 4p