Zobrazeno 1 - 10
of 27
pro vyhledávání: '"G. N. Dudin"'
Autor:
N. I. Batura, G. N. Dudin
Publikováno v:
Doklady Physics. 67:477-479
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1902aeba4d761ad599d368d660ca64c9
https://doi.org/10.1134/s1028335822120011
https://doi.org/10.1134/s1028335822120011
Autor:
G. N. Dudin
Publikováno v:
Fluid Dynamics. 57:247-260
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7018b6013b5226aac6b4914eb8c59568
https://doi.org/10.1134/s0015462822030053
https://doi.org/10.1134/s0015462822030053
Publikováno v:
Fluid Dynamics. 56:219-227
The results of an experimental wind-tunnel investigation of the plate surface heating in the strong viscous-inviscid interaction regime are presented. It is shown that In the presence of a wedge mounted in the vicinity of the trailing edge of the pla
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ee9ad0b7686b115ece35cc2508dd0585
https://doi.org/10.1134/s0015462821020038
https://doi.org/10.1134/s0015462821020038
Autor:
V. V. Bashkatov, G. N. Dudin
Publikováno v:
Proceedings of Moscow Institute of Physics and Technology. 13:86-96
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0258ae7693ff8ab3076c84167e25ee0b
https://doi.org/10.53815/20726759_2021_13_4_86
https://doi.org/10.53815/20726759_2021_13_4_86
Autor:
G. N. Dudin, V. Ya. Neyland
Publikováno v:
Доклады Академии наук. 487:24-27
The flow around the yawed plate in the regime of strong interaction is considered in the case when the pressure at its trailing edge is not constant, but changes along the transverse coordinate. It is shown that in the case of large transverse gradie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::965c36bf4e177cc2583efed02917930b
https://doi.org/10.31857/s0869-5652487124-27
https://doi.org/10.31857/s0869-5652487124-27
Autor:
A. V. Ledovskii, G. N. Dudin
Publikováno v:
Fluid Dynamics. 54:472-480
The flow in the three-dimensional laminar boundary layer in the vicinity of the plane of symmetry of a semi-infinite planar wing having a bend of the leading edge is investigated in the case of strong interaction with the external hypersonic flow. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4fde70d1e47a9b6978fcbca51d80e742
https://doi.org/10.1134/s0015462819030030
https://doi.org/10.1134/s0015462819030030
Autor:
G. N. Dudin, V. Ya. Neyland
Publikováno v:
Doklady Physics. 63:467-470
Hypersonic flow past a yawed plate of finite length is considered in the regime of strong interaction for the case when an additional condition at its trailing edge varies in span instead of being constant. It is shown that, in this case, the form of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ab20818e5cc257c67ab09f83a3a9177a
https://doi.org/10.1134/s1028335818110010
https://doi.org/10.1134/s1028335818110010
Autor:
G. N. Dudin, A. A. Balashov
Publikováno v:
Fluid Dynamics. 53:394-401
Viscous gas flow past a finite-length plate in the strong interaction regime is investigated. The expansions of the flow functions in the vicinity of the leading edge are derived and the boundary value problems for the viscous and inviscid flow regio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e70ce3f58d449fa0dfc12b5ff6b7db1f
https://doi.org/10.1134/s0015462818030035
https://doi.org/10.1134/s0015462818030035
Autor:
F. H. Nguen, G. N. Dudin
Publikováno v:
Fluid Dynamics. 50:522-534
Three-dimensional laminar boundary layer flow over a planar delta wing with the span of the order of unity is investigated in the strong interaction regime. The flow functions are expanded in power series in the transverse coordinate in the vicinitie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5cebe4302b617f3f22fc5c179afb3264
https://doi.org/10.1134/s0015462815040079
https://doi.org/10.1134/s0015462815040079
Autor:
K. T. M’int, G. N. Dudin
Publikováno v:
Fluid Dynamics. 45:422-433
The propagation of perturbations in the three-dimensional boundary layer on a planar delta wing in a hypersonic gas stream is investigated in the strong viscid-inviscid interaction regime. A characteristic associated with the induced pressure is foun
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2447033e2b343368b707d267e3a3c2e1
https://doi.org/10.1134/s0015462810030099
https://doi.org/10.1134/s0015462810030099