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Modified Patterson temperature jump condition considering viscous heat generation.

Authors :
Le, Nam T.P.
Tran, Nam H.
Tran, Thoai N.
Source :
International Journal of Heat & Mass Transfer. Nov2018:Part B, Vol. 126, p1267-1274. 8p.
Publication Year :
2018

Abstract

Highlights • Effects of slip velocity and wall temperature on temperature jump condition are investigated. • Modified Patterson temperature jump condition is proposed by involving viscous heat generation. • This modified jump condition can predict the surface gas temperature for the airfoil case Kn = 0.26. Abstract Recently, new type of the Smoluchowski temperature jump condition has been proposed by considering viscous heat generation in rarefied gas flow simulations, and improved prediction of the surface gas temperature in comparing with DSMC data. Two forms of the Patterson jump condition have been revisited for rarefied gas flow simulations in the literature. In this paper, the modified Patterson temperature jump condition is proposed by considering viscous heat generation. We numerically investigate the effect of the slip velocity, the wall temperature and viscous heat generation on the surface gas temperature for external high-speed rarefied gas flow simulations by using various forms of the Patterson jump condition. Three configurations such as the sharp leading-edge flat plate, the sharp 25–55-deg biconic, and micro-airfoil NACA0012 are selected for simulations with Mach number from 2 to 15.6, and Knudsen number ranging from 0.04 to 0.26. The simulation results obtained show that the modified Patterson jump condition gives good agreement with the DSMC data, and predict temperatures better than those of new type of the Smoluchowski jump condition for all cases considered. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
00179310
Volume :
126
Database :
Academic Search Index
Journal :
International Journal of Heat & Mass Transfer
Publication Type :
Academic Journal
Accession number :
131771936
Full Text :
https://doi.org/10.1016/j.ijheatmasstransfer.2018.06.046