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Wall heat transfer of unsteady near-wall flow in internal combustion engines

Authors :
Hidefumi Fujimoto
Kiyotaka Sato
Qianjin Zhu
Mamoru Tanahashi
Tatsuya Tanaka
Yuji Harada
Hiroyuki Yamashita
Kenji Uchida
Source :
International Journal of Engine Research. 20:817-833
Publication Year :
2019
Publisher :
SAGE Publications, 2019.

Abstract

Although the near-wall turbulence is not fully developed in the engine combustion chamber, wall heat transfer models based on flow characteristics in fully developed near-wall turbulence are typically employed in engine simulations to predict heat transfer. Only few studies reported the wall heat transfer mechanism in near-wall flow where the near-wall turbulence was not fully developed as expected in the engine combustion chamber. In this study, the velocity distribution and wall heat flux in such a near-wall flow were evaluated using a rapid compression and expansion machine. In addition to the experimental approach, a numerical simulation with highly resolved calculation mesh was applied in various flow fields expected in the engine combustion chamber. As a result, the turbulent Reynolds number that represents the relationship between turbulent production and dissipation varied in the wall boundary layer according to the near-wall flow condition. This behavior affects the wall heat transfer. Considering this finding, a new model was formulated by introducing a ratio of turbulent Reynolds number in an intended near-wall flow to that in fully developed near-wall turbulence. It was confirmed that the proposed model could improve the prediction accuracy of wall heat flux even in near-wall flow where the near-wall turbulence was not fully developed. By applying the proposed model in engine computational fluid dynamics, it was found that the proposed model could predict the wall heat flux in a homogeneous charge compression ignition gasoline engine with acceptable accuracy.

Details

ISSN :
20413149 and 14680874
Volume :
20
Database :
OpenAIRE
Journal :
International Journal of Engine Research
Accession number :
edsair.doi...........6b9485fa752479fcba09fcac10d55fbd
Full Text :
https://doi.org/10.1177/1468087419853432