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Peculiarities of flowand heat transfer in the base area of interplanetary probes
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This article is published in Tsagi Science Journal.The article was published on 2010-01-01. It has received 2 citations till now. The article focuses on the topics: Stanton number & Heat flux.read more
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Numerical Study of the Supersonic Base Flow around Aircraft Model
TL;DR: In this paper, a numerical study of the base part of the supersonic flow past an aircraft model was carried out using the software developed by the authors for calculating 3D turbulent flow of viscous compressible gas in the framework of the unsteady Reynolds averaged Navier-Stokes equations (URANS) with the Spalart-Allmaras (SA) and Menter's SST turbulence models.
Experimental researches in high temperature facilities of TsAGI
TL;DR: In this paper, the main results of certain experimental investigations, which have been implemented in recent years in high-speed high-temperature and high-enthalpy wind tunnels of the Central Aerohydrodynamic Institute (TsAGI), are presented, including 1 Heat exchange at a laminar1turbulent transition on a sharp cone; 1 Flow and heat exchange on a body surface at the incidence of the shock wave; and 1 Flow exchange at tangential blow of gas into a wall layer of the body in flow (including the dust-laden layer) through a