ENHANCEMENT OF HEAT TRANSFER THROUGH A SUDDEN EXPANSION PIPE AIRFLOW USING PROPELLER SWIRL GENERATOR
Zohir, A., Gomaa, A. (2012). ENHANCEMENT OF HEAT TRANSFER THROUGH A SUDDEN EXPANSION PIPE AIRFLOW USING PROPELLER SWIRL GENERATOR. EKB Journal Management System, 40(No 4), 1039-1055. doi: 10.21608/jesaun.2012.114476
A. E. Zohir; A.G. Gomaa. "ENHANCEMENT OF HEAT TRANSFER THROUGH A SUDDEN EXPANSION PIPE AIRFLOW USING PROPELLER SWIRL GENERATOR". EKB Journal Management System, 40, No 4, 2012, 1039-1055. doi: 10.21608/jesaun.2012.114476
Zohir, A., Gomaa, A. (2012). 'ENHANCEMENT OF HEAT TRANSFER THROUGH A SUDDEN EXPANSION PIPE AIRFLOW USING PROPELLER SWIRL GENERATOR', EKB Journal Management System, 40(No 4), pp. 1039-1055. doi: 10.21608/jesaun.2012.114476
Zohir, A., Gomaa, A. ENHANCEMENT OF HEAT TRANSFER THROUGH A SUDDEN EXPANSION PIPE AIRFLOW USING PROPELLER SWIRL GENERATOR. EKB Journal Management System, 2012; 40(No 4): 1039-1055. doi: 10.21608/jesaun.2012.114476

ENHANCEMENT OF HEAT TRANSFER THROUGH A SUDDEN EXPANSION PIPE AIRFLOW USING PROPELLER SWIRL GENERATOR

JES. Journal of Engineering Sciences
Article 6, Volume 40, No 4, July and August 2012, Page 1039-1055  XML PDF (517.04 K)
Document Type: Research Paper
DOI: 10.21608/jesaun.2012.114476
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Authors
A. E. Zohir1; A.G. Gomaa2
1Mechanical Engineering Department, Tabbin Institute for Metallurgical Studies, Cairo, Egypt,
2Mechanical Eng. Dept., Industrial education College, Helwan University
Abstract
This investigation is aimed to study the heat transfer and pressure drop characteristics for turbulent airflow in a sudden expansion pipe (d/D = 0.72) equipped with propeller swirl generator with different blade angles. The investigation is performed for the Reynolds number ranging from 10,000 to 40,000 under a uniform heat flux condition. Four propeller fans of five blades with swirl angles, Ө = 15, 30, 45° for upstream flow, and 45° for downstream flow are inserted separately inside the test section. The swirl propeller fan is located at different locations inside the tested pipe, where S =10H, 20H and 40H for both upstream and downstream flows. The experimental results indicate that inserting the propeller upstream of the tube provides considerable improvement of the heat transfer rate up to 190% for all swirler angles with higher values obtained at Ө = 45°. Inserting the propeller downstream of the tube provides more improvement in heat transfer rate than inserting the propeller upstream of the tube at swirl angle of Ө = 45°, the heat transfer rate increased up to 225%. The maximum enhancement efficiency (η) for the downstream swirler is about 326% while it is about 213% for the upstream one. Correlations for relative mean Nusselt number and enhancement efficiency are presented for different fan locations, swirl angles and Reynolds numbers.
Keywords
sudden expansion; swirl flow; heat transfer augmentation
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