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Teplofizika vysokikh temperatur, 2001, Volume 39, Issue 4, Pages 581–588 (Mi tvt1937)  
Heat and Mass Transfer and Physical Gasdynamics

Effect of the temperature drop between the isothermic walls of a channel on the structure of supersonic flow and on the aerodynamic properties

V. A. Bashkin, I. V. Egorov, D. V. Ivanov

Central Aerohydrodynamic Institute, Zhukovskii
Full-text PDF (2237 kB)
Abstract: The results of numerical analysis of the two-dimensional Navier-Stokes equations are used to investigate a supersonic flow of a perfect gas in a symmetric plane channel of variable cross section at the Mach number of $\mathrm{M}_\infty=4$ at the inlet for the Reynolds numbers in the range $\mathrm{Re}=10^3-10^6$. The top and bottom channel walls are assumed to be isothermic with different values of the temperature factor. It is shown that the asymmetry of the boundary conditions for temperature leads to the asymmetry of the entire flow field.
Received: 15.09.2000
English version:
High Temperature, 2001, Volume 39, Issue 4, Pages 540–547
DOI: https://doi.org/10.1023/A:1017936223438
Bibliographic databases:
Document Type: Article
UDC: 533.6.011.8
Language: Russian
Citation: V. A. Bashkin, I. V. Egorov, D. V. Ivanov, “Effect of the temperature drop between the isothermic walls of a channel on the structure of supersonic flow and on the aerodynamic properties”, TVT, 39:4 (2001), 581–588; High Temperature, 39:4 (2001), 540–547
Citation in format AMSBIB
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\paper Effect of the temperature drop between the isothermic walls of a channel on the structure of supersonic flow and on the aerodynamic properties
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\yr 2001
\vol 39
\issue 4
\pages 581--588
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\jour High Temperature
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