Effect of surface roughness on the oil distribution and the heat transfer coefficient for piston cooling gallery

Piston cooling gallery plays a critical role in managing the temperature of the piston and its performance. This paper aims to study the effect of surface roughness on heat transfer coefficient (HTC) inside the cooling gallery. To do so, Eulerian multiphase model and the k-ε turbulence model were us...

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Bibliographic Details
Main Authors: Hamza, M. (Author), Mei, B.-A (Author), Zuo, Z. (Author)
Format: Article
Language:English
Published: Elsevier Ltd 2022
Subjects:
Online Access:View Fulltext in Publisher
LEADER 02536nam a2200421Ia 4500
001 0.1016-j.csite.2022.101960
008 220421s2022 CNT 000 0 und d
020 |a 2214157X (ISSN) 
245 1 0 |a Effect of surface roughness on the oil distribution and the heat transfer coefficient for piston cooling gallery 
260 0 |b Elsevier Ltd  |c 2022 
856 |z View Fulltext in Publisher  |u https://doi.org/10.1016/j.csite.2022.101960 
520 3 |a Piston cooling gallery plays a critical role in managing the temperature of the piston and its performance. This paper aims to study the effect of surface roughness on heat transfer coefficient (HTC) inside the cooling gallery. To do so, Eulerian multiphase model and the k-ε turbulence model were used for the oil and air flow through the cooling gallery. Dimples and protrusions were considered inside the cooling gallery for roughness. The results indicate that roughness elements distorted the oil distribution resulting in weaker oil slug formation and faster oil slug diffusion with the oil collected along the top or bottom wall. In addition, the average HTC for the walls was highly dependent on the jet impingement near the inlet. The average HTC didn't show much variation trend for the top and inner wall but there was prominent variation trend for the bottom and the outer wall. Moreover, vortex was observed within the dimple roughness element which resulted in rebounding effect leaving a trail of low HTC right behind the dimple roughness element. This was absent for protrusion roughness element. Finally, the oil flow across the protrusion led to higher local HTC compared with dimple roughness elements. © 2022 The Authors 
650 0 4 |a Average heat transfers 
650 0 4 |a Cooling 
650 0 4 |a Eulerian 
650 0 4 |a Heat transfer coefficient 
650 0 4 |a Heat transfer coefficients 
650 0 4 |a Heat transfer co-efficients 
650 0 4 |a Multiphase 
650 0 4 |a Multiphases 
650 0 4 |a Oil distributions 
650 0 4 |a Oil flow 
650 0 4 |a Oil oscillation 
650 0 4 |a Oil oscillation 
650 0 4 |a Oscillating flow 
650 0 4 |a Performance 
650 0 4 |a Piston cooling gallery 
650 0 4 |a Piston cooling gallery 
650 0 4 |a Pistons 
650 0 4 |a Roughness elements 
650 0 4 |a Surface roughness 
650 0 4 |a Surface roughness 
650 0 4 |a Turbulence 
650 0 4 |a Turbulence models 
700 1 0 |a Hamza, M.  |e author 
700 1 0 |a Mei, B.-A.  |e author 
700 1 0 |a Zuo, Z.  |e author 
773 |t Case Studies in Thermal Engineering