Zobrazeno 1 - 10
of 17
pro vyhledávání: '"V. Ya. Borovoi"'
Publikováno v:
Fluid Dynamics. 46:917-934
The results of an experimental and numerical investigation of flow and heat transfer in the region of the interaction between an incident oblique shock and turbulent boundary layers on sharp and blunt plates are presented for the Mach numbers M∞ =
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7054b0a6e8d54f29440c0960eac94cf8
https://doi.org/10.1134/s0015462811060093
https://doi.org/10.1134/s0015462811060093
Publikováno v:
Doklady Physics. 50:3-6
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3f2abcf8cde2abf12b90117993349a3a
https://doi.org/10.1134/1.1862364
https://doi.org/10.1134/1.1862364
Autor:
T. V. Kubyshina, V. Ya. Borovoi
Publikováno v:
Fluid Dynamics. 28:171-176
The flow and heat transfer on the windward surface of tail fins has been experimentally investigated for Mach numbersM∞ =5 and 8 and Re∞L=(0.6−1.1)·106 (L is the length of the central chord of the wing on which the fins are mounted). Two lines
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0fb3a26262fcbf20f6ca7280ac8c7ea4
https://doi.org/10.1007/bf01051203
https://doi.org/10.1007/bf01051203
Autor:
V. Ya. Borovoi, L. V. Yakovlev
Publikováno v:
Fluid Dynamics. 26:676-680
The flow and heat transfer on a plate with a single spherical cavity has been experimentally investigated for M∞=4 and Re∞,L=3.1 · 106. The flow pattern over the cavity has been obtained. Zones of enhanced heat transfer have been detected, and t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8cea06ea829a49c2ca3f1ae7caef9dfd
https://doi.org/10.1007/bf01050986
https://doi.org/10.1007/bf01050986
Autor:
I. V. Struminskaya, V. Ya. Borovoi
Publikováno v:
Fluid Dynamics. 26:415-420
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2df0035fb891dec0fef8235f93e4a0da
https://doi.org/10.1007/bf01059014
https://doi.org/10.1007/bf01059014
Publikováno v:
Separated Flows and Jets ISBN: 9783642844492
Using various experimental methods the “architecture” of the separated flows formed at the lee-side of a blunt cone and delta wing is investigated. The flow structure evolution during the variation of the angle of attack and the Mach number is di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1ec6cfc7559af12b209d59ee61d49d1
https://doi.org/10.1007/978-3-642-84447-8_40
https://doi.org/10.1007/978-3-642-84447-8_40
Publikováno v:
Fluid Dynamics. 17:361-367
A detailed investigation of the heat transfer is made for the case of a turbulent boundary layer on a cone in front of a cylindrical obstacle.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4df359bfe0b11f3236d4fe669d2733f0
https://doi.org/10.1007/bf01091271
https://doi.org/10.1007/bf01091271
Autor:
V. Ya. Bezmenov, L. A. Pleshakova, M. M. Ardasheva, V. Ya. Borovoi, M. V. Ryzhkova, V. V. Osipov
Publikováno v:
Fluid Dynamics. 14:820-824
A brief description is given of the method used to measure the heat flux in a shock tube by means of coverings that indicate the heat flux and by means of microthermocouples. The distribution of the heat flux was investigated and some data were obtai
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::adbf572e9492eb30ee9324bf205b417f
https://doi.org/10.1007/bf01051981
https://doi.org/10.1007/bf01051981
Publikováno v:
Fluid Dynamics. 11:736-739
Results are given of an investigation of heat transfer on the flat surface of a blunted half-cone, washed at zero angle of attack by a helium flow at high Mach number (up to 23.5). A correlation is given for the experimental data obtained over a wide
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5cd10b31abb7f0e9094a675f2223d4b
https://doi.org/10.1007/bf01012967
https://doi.org/10.1007/bf01012967
Publikováno v:
Fluid Dynamics. 17:513-519
To establish the influence of the unit Reynolds number on the transition of a boundary layer on the side surface of a cone, the transition was investigated on a model of a sharp cone with half-angle θ = 7.5 ° and lengths from 150 to 400 mm. The exp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79ab1f4709d0ef56020642a3d26f81d4
https://doi.org/10.1007/bf01090017
https://doi.org/10.1007/bf01090017