Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Pavel Polivanov"'
Publikováno v:
Aerospace, Vol 10, Iss 9, p 798 (2023)
The paper focuses on the investigation of unsteady effects in shock wave/boundary layer interaction. The study was carried out using a flat plate model subjected to a free stream Mach number of 1.43 and a unit Reynolds number (Re1) of 11.5 × 106 1/m
Externí odkaz:
https://doaj.org/article/0983d7153dd64de28b2300b772afdf57
Publikováno v:
Aerospace, Vol 10, Iss 4, p 363 (2023)
The problem of flow control under conditions of a turbulent boundary layer at transonic and supersonic free-stream velocities is considered. Such flows are integral components of the flight process and exert significant effects on the flow around bot
Externí odkaz:
https://doaj.org/article/161bae8cb78546febf61a9b254453ac2
Publikováno v:
30th International Symposium on Shock Waves 2 ISBN: 9783319448640
Modern trends in transonic aviation are connected with reducing viscous drag. Therefore commercial airplanes of the next generation may be equipped with a laminar wing [1, 2]. Generic feature of the transonic flow near the airfoil is presence of loca
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04a2dde2c6e6133ea21f4a1799e05131
https://doi.org/10.1007/978-3-319-44866-4_62
https://doi.org/10.1007/978-3-319-44866-4_62
Publikováno v:
30th International Symposium on Shock Waves 2 ISBN: 9783319448640
The study is relevant to plasma flow control applications, namely, delay of buffet onset of transonic airfoils using plasma discharges. At transonic speeds the region of supersonic flow arises on the suction side of the airfoil ended by the strong sh
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::022b658e1ffcf443e57c2ab1f9556918
https://doi.org/10.1007/978-3-319-44866-4_75
https://doi.org/10.1007/978-3-319-44866-4_75
Publikováno v:
Siberian Journal of Physics. 3:3-14
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::652ee4702fbd64684b9d99521c4d3f41
https://doi.org/10.54362/1818-7919-2008-3-2-3-14
https://doi.org/10.54362/1818-7919-2008-3-2-3-14
Autor:
Pavel Polivanov
Publikováno v:
MATEC Web of Conferences, Vol 115, p 02011 (2017)
The effect of blowing/suction through perforated surfaces on the turbulent boundary layer was studied experimentally at Mach number M = 1.4. In the experiments, several different porous surfaces were investigated in a wide range of the blowing/suctio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4095cb8cc5654e63fab09c2c8d0127ee
https://doi.org/10.1051/matecconf/201711502011
https://doi.org/10.1051/matecconf/201711502011