Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Y A, Vinogradov"'
Autor:
Y. A. Vinogradov
Publikováno v:
Eurasia from the Aeneolithic (Chalcolithic) Era to the Early Middle Ages (Innovations, Contacts, Transmission of Ideas and Technologies). Материалы международной научной конференции, посвященной 120-летию со дня рождения выдающегося исследователя древностей Южной Сибири и Центральной Азии Михаила Петровича Грязнова (1902-1984).
Publikováno v:
Experimental Thermal and Fluid Science. 88:202-219
The process of energy (temperature) separation in an airflow is experimentally investigated in a device consisting of two coaxial channels with heat-conducting walls. The air flows at a supersonic velocity along the inner channel and at a subsonic ve
Publikováno v:
Journal of Physics: Conference Series. 1683:022064
The results of an experimental study of the thermal parameters of a supersonic flow around a flat wall in the presence of finely divided water droplets are presented. The relative mass flow rate of the liquid (mass concentration) varied in the range
Publikováno v:
Journal of Physics: Conference Series. 1392:012077
The article puts forward a modified finite element method based on decomposition and analytical solution techniques. The algorithm is as follows. A complex structure is divided into simple form sub-regions which involve partial differential equations
Publikováno v:
Journal of Physics: Conference Series. 1369:012040
The results of an experimental study of heat transfer for a supersonic flow behind a backward-facing step are presented. Input flow Mach number was 2.2, Reynolds number was over 20 million when calculated with the use of the dynamic boundary layer le
Publikováno v:
Journal of Physics: Conference Series. 1129:012022
Publikováno v:
Journal of Physics: Conference Series. 891:012080
Experimental results for artificially initiated shock wave influence on machineless gas flow energy separation effect are presented. The working principle of the technique is based on interaction of supersonic and subsonic flows through the heat-cond
Publikováno v:
EPJ Web of Conferences, Vol 159, p 00030 (2017)
Investigations of supersonic air flow around plane surface behind a rib perpendicular to the flow direction are performed. Research was carried out for free stream Mach number 2.25 and turbulent flow regime - Rex >2·107 . Rib height was varied in ra
The ratios of yields of anti-baryons to baryons probes the mechanisms of baryon-number transport. Results for (p) over bar /p, (Lambda) over bar/Lambda, (Xi) over bar (+)/(Xi) over bar (-) and (Omega) over bar (+)/(Omega) over bar (-) in pp collision
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2127::99fb9d8373f09e076e30483aa9f0c869
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3158103
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3158103
In this paper measurements are presented of pi(+/-), K-+/-, p, and (p) over bar production at midrapidity (vertical bar y vertical bar < 0.5), in Pb-Pb collisions at root s(NN) = 2.76 TeV as a function of centrality. The measurement covers the transv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2127::ad92e7236812b766c5278c09542694eb
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3159084
https://pergamos.lib.uoa.gr/uoa/dl/object/uoadl:3159084