Journal of Jilin University(Engineering and Technology Edition) ›› 2021, Vol. 51 ›› Issue (5): 1557-1564.doi: 10.13229/j.cnki.jdxbgxb20200598

   

Investigation on influence of cooling tube structure and airflow speed on cold side performance of air⁃cooled charge air cooler

Xing-jun HU(),Jing-long ZHANG,Li XIN,Yu-fei LUO,Jing-yu WANG,Tian-ming YU()   

  1. State Key Laboratory of Automotive Simulation and Control,Jilin University,Changchun 130022,China
  • Received:2020-04-12 Online:2021-09-01 Published:2021-09-16
  • Contact: Tian-ming YU E-mail:hxj@jlu.edu.cn;yutm@jlu.edu.cn

Abstract:

Based on the existed experimental results, this paper applies the Computational Fluid Dynamics (CFD) to investigate the leading edge structure of the cooling tube and airflow speed on the thermal-hydraulic performance of an air-cooled charge air cooler (ACAC). Results showed that, under the same fillet radius R1 the Fanning friction factor f raises with the increasing airflow speed, but at the same airflow speed f decreases with the increasing of R1, when taking R1=0.9 mm as a baseline, the f of R1=0 mm increased at a maximum of 12.42%, the f of R1=3.6 mm deceased at a maximum of 5.41%; For the Nusselt number Nu, under the same fillet radius R1 it raises with the increasing airflow speed, but at the same airflow speed it decreases with the increasing of R1, also taking R1=0.9 mm as a baseline, the Nu of R1=0 mm increases at a maximum of 2.22 % and the Nu of R1=3.6 mm decreases at a maximum of 1.49 %; For PEC, under the same fillet radius R1 it raises with the increasing airflow speed, and at the same airflow speed, it also increases with the increasing of R1, again taking R1=0.9 mm as a baseline, the PEC value of R1=0 mm decreases at a maximum of 10.13 % and increases at a maximum value of 3.4 % when R1=3.6 mm. In summary, when R1=3.6 mm, airflow speed equals 7.5 m/s, the ACAC achieves its best thermal-hydraulic performance, therefore, increasing R1 and airflow speed is helpful to improve the thermal-hydraulic performance of ACAC.

Key words: mechanical engineering, air-cooled charge air cooler, leading edge structure of cooling tube, airflow speed, computational fluid dynamics, thermal-hydraulic performance

CLC Number: 

  • U461.8

Fig.1

Air-cooled charge air cooler"

Table 1

Structural parameters"

参数数值参数数值
冷却管长度Lt/mm604翅片厚度tLF/mm0.1
冷却管宽度Wt/mm50翅片高度hLF/mm12
冷却管高度Ht/mm8百叶间距Lp/mm3
开窗角度φ/(°)20翅片长度LLF/mm50
翅片间距pLF/mm2.75开窗高度lh/mm1.1

Fig.2

Test facility"

Fig.3

Computational domain"

Fig.4

Different leading edge structures of flat cooling tube"

Fig.5

Comparison of static pressure drop"

Fig.6

Relationship between f and velocity under different R1"

Fig.7

Velocity at middle XY Plane under different R1 at 7.5 m/s"

Fig.8

Pressure along middle line AB under different R1 at 7.5 m/s"

Fig.9

Relationship between Nu and velocity under different R1"

Fig.10

Temperature at the middle XY Plane under different R1 at 7.5 m/s"

Fig.11

Relationship between PEC and velocity under different R1"

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