Zobrazeno 1 - 10 of 21 pro vyhledávání: '"S. S. Popovich"'
4
Measurement of the Adiabatic Wall Temperature of a Flat Plate in a Supersonic Air-Droplet Flow
Autor: S. S. Popovich, N. V. Medvetskaya, Yu. A. Vinogradov, N. A. Kiselev, A G Zditovets
Publikováno v: Fluid Dynamics. 55:701-707
The results of the measurement of the surface temperature of a flat plate in a supersonic air-droplet flow are presented. The plate made of duralumin was mounted vertically in the working channel of an aerodynamic setup. The droplets of a liquid (dis
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::e0e8c5a4bf35f1e5420f8ae7853191db
https://doi.org/10.1134/s0015462820050146
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6
The effect of the initial swirl of the supersonic flow of humid air on the adiabatic wall temperature
Autor: N. A. Kiselev, Yu A Vinogradov, A G Zditovets, S S Popovich
Publikováno v: Journal of Physics: Conference Series. 2088:012056
The paper presents the results of measuring the adiabatic wall temperature of an axisymmetric channel during acceleration of the moist air flow in it to supersonic speed. The initial swirl was imparted to the flow (swirling parameter S = 0.5, 1.0, 2.
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f715404cd960da863a357097827497e8
https://doi.org/10.1088/1742-6596/2088/1/012056
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8
Heat transfer and skin-friction in a turbulent boundary layer under a non-equilibrium longitudinal adverse pressure gradient
Autor: Alexander I. Leontiev, A G Zditovets, S. S. Popovich, N. A. Kiselev, Yu. A. Vinogradov
Publikováno v: International Journal of Heat and Fluid Flow. 89:108801
The experimental data on the effect of weak and moderate non-equilibrium adverse pressure gradients (APG) on the parameters of dynamic and thermal boundary layers are presented. The Reynolds number based on the momentum thickness at the beginning of
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::269adcbfc5b2dfb1d6e9ee754ed2fd0f
https://doi.org/10.1016/j.ijheatfluidflow.2021.108801
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9
Experimental study of the shock wave influence on adiabatic wall temperature in a supersonic air-droplet flow
Autor: S S Popovich, A G Zditovets, N. A. Kiselev, Y. A. Vinogradov
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
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::6c739a15ad1817c613d2e9aa18081b2a
https://doi.org/10.1088/1742-6596/1683/2/022064
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