Zobrazeno 1 - 8
of 8
pro vyhledávání: '"V. Ya. Borovoy"'
Autor:
Vladimir Nikolaevich Radchenko, Herbert Olivier, P. V. Chuvakhov, Amit Roghelia, V. Ya. Borovoy, Ivan Vladimirovich Egorov
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 58:975-989
The influence of small cylindrical bluntness of the leading edge of a flat plate on formation of spatial structures in a nominally two-dimensional supersonic compression corner flow at the Mach number M∞ ≈ 8 and a laminar state of the undisturbed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1d3cf4793f335d8a08daeeada50624c
https://doi.org/10.1134/s0021894417060037
https://doi.org/10.1134/s0021894417060037
Autor:
A. S. Skuratov, Vladimir Nikolaevich Radchenko, Vladimir Evguenyevich Mosharov, I. V. Struminskaya, V. Ya. Borovoy
Publikováno v:
Fluid Dynamics. 49:454-467
Flow in an idealized air-inlet with plane walls and a rectangular cross-section is experimentally investigated. The air-inlet is mounted on a plate, at a distance well removed from its leading edge. The experiments were conducted in a Ludwig tube at
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7d919576fd871c7c08f872ca950a775e
https://doi.org/10.1134/s0015462814040061
https://doi.org/10.1134/s0015462814040061
Autor:
Ivan Vladimirovich Egorov, Vladimir Nikolaevich Radchenko, A. S. Skuratov, I. V. Struminskaya, Vladimir Evguenyevich Mosharov, V. Ya. Borovoy
Publikováno v:
Fluid Dynamics. 48:636-647
Gas flow and heat transfer on the surfaces of sharp and blunt plates is experimentally investigated in the presence of two forward-looking wedges at the Mach numbers M = 5, 6, and 8 and the Reynolds numbers up to Re∞L = 27×106. It is shown that th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9b7638215e253399c327177148a7cfe7
https://doi.org/10.1134/s0015462813050074
https://doi.org/10.1134/s0015462813050074
Publikováno v:
TsAGI Science Journal. 41:227-257
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8d35795d8a5f3ee4eedfe1208d96f277
https://doi.org/10.1615/tsagiscij.v41.i3.10
https://doi.org/10.1615/tsagiscij.v41.i3.10
Publikováno v:
Fluid Dynamics. 43:369-379
The heat transfer to sharp and slightly blunted flat plates in the zone of oblique shock incidence has been experimentally investigated. The experiments were performed at the Mach numbers M = 6, 8, and 10 and Reynolds numbers ranging from 0.2 × 106
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ebf8ef78302c106f529facb8036397e
https://doi.org/10.1134/s0015462808030058
https://doi.org/10.1134/s0015462808030058
Publikováno v:
Journal of Spacecraft and Rockets. 38:249-256
Consideration is given to the experimental investigation of the original method of providing radio communications with a reentry vehicle along the trajectory section when a vehicle is surrounded by plasma of the ionized shock layer. The method sugges
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b750b9217e047d6a24253ddf2cea3ebf
https://doi.org/10.2514/2.3678
https://doi.org/10.2514/2.3678
Publikováno v:
Fluid Dynamics. 35:682-691
The dissipation of a tip vortex generated by a rectangular wing and the stagnation pressure and temperature distributions within the vortex are experimentally investigated. The interaction of the vortex with the bow shock ahead of a sphere and the he
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cac68ca2955aad834071f42c3eab5164
https://doi.org/10.1023/a:1026686730879
https://doi.org/10.1023/a:1026686730879
Publikováno v:
Scopus-Elsevier
Hypersonic flows are prone to intense shock waves whose intersection, or interference, gives rise to a system of waves and slip surfaces that can have a large influence on the aerodynamics of a vehicle. It is convenient to distinguish six types of in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::32300ab071095d138351ba862a5dcf2f
https://doi.org/10.2514/2.41
https://doi.org/10.2514/2.41