Zobrazeno 1 - 10
of 32
pro vyhledávání: '"Yermolaev Yury"'
Publikováno v:
EPJ Web of Conferences, Vol 196, p 00017 (2019)
The influence of the parameters of the impulse action on the laminar supersonic flat-plate boundary layer on the excited localized perturbations is investigated at Mach 2. The influence of the duration of a pulsed discharge on the generated disturban
Externí odkaz:
https://doaj.org/article/080c5a59aca34f30bd6663180b34306d
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
Akademický článek
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Akademický článek
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Autor:
KOSINOV, Alexander, SEMIONOV, Nikolai, PANINA, Alexandra, KOLOSOV, Gleb, YATSKIKH, Aleksey, YERMOLAEV, Yury
Experiments on the disturbance evolution are conducted in boundary layer of 45-degrees swept-wing with periodic roughness elements at Mach 2 and 2.5. Flow characteristics are measured by constant temperature anemometer. For disturbance quantities def
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77ddcabf3d2612b7a6e634923a2400a8
Autor:
KOSINOV, Alexander, SEMIONOV, Nikolai, KOLOSOV, Gleb, PANINA, Alexandra, YERMOLAEV, Yury, YATSKIKH, Aleksey
Origin of the streaks are examined in fat plate boundary layer at Mach 2 and 2.5. They arise due to the interaction of the weak shock waves with flow in vicinity of the flat plate leading edge. The process is accompanied by significant increasing of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cf29741ed4c959963e43bcf37cab94c2
Autor:
YATSKIKH, Alexey, YERMOLAEV, Yury, KOSINOV, Alexander, SEMIONOV, Nikolai, SEMENOV, Alexander, RUMENSKIKH, Marina
The evolution of a controlled broadband wave packet in flat-plate and swept-wing supersonic boundary layers was experimentally investigated at Mach number M=2. The wave packet was introduced into the boundary layer by a localized pulse electrical dis
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8c2dc87e8bda9590db8e1dfe66ef622f
Autor:
Markovich, D.M., Kuibin, P.A., Vorobyev, M.A., Yatskikh, Aleksey, Semenov, Aleksander, Kolosov, Gleb, Kosinov, Aleksander, Yermolaev, Yury
Publikováno v:
EPJ Web of Conferences; 2019, Vol. 196, pN.PAG-N.PAG, 4p
Publikováno v:
AIP Conference Proceedings; 2018, Vol. 2036 Issue 1, p030102-1-030102-9, 9p