High-porosity metal foams are known for providing high heat transfer rates, as they provide a significant increase in wetted surface area as well as highly tortuous flow paths resulting in enhanced mixing. Further, jet impingement offers high convective cooling, particularly at the jet footprint areas on the target surface due to flow stagnation. In this study, high-porosity thin metal foams were subjected to array jet impingement, for a special crossflow scheme. High porosity (92.65%), high pore density (40 pores per inch (ppi)), and thin foams (3 mm) have been used. In order to reduce the pumping power requirements imposed by full metal foam design, two striped metal foam configurations were also investigated. For that, the jets were arranged in 3 × 6 array (x/dj = 3.42, y/dj = 2), such that the crossflow is dominantly sideways. Steady-state heat transfer experiments have been conducted for varying jet-to-target plate distance z/dj = 0.75, 2, and 4 for Reynolds numbers ranging from 3000 to 12,000. The baseline case was jet impingement onto a smooth target surface. Enhancement in heat transfer due to impingement onto thin metal foams has been evaluated against the pumping power penalty. For the case of z/dj = 0.75 with the base surface fully covered with metal foam, an average heat transfer enhancement of 2.42 times was observed for a concomitant pressure drop penalty of 1.67 times over the flow range tested.
Skip Nav Destination
Article navigation
December 2019
Research-Article
Jet Impingement Heat Transfer Enhancement by Packing High-Porosity Thin Metal Foams Between Jet Exit Plane and Target Surface
Srivatsan Madhavan,
Srivatsan Madhavan
Department of Mechanical and Aerospace Engineering,
911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: smadhav5@ncsu.edu
North Carolina State University
,911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: smadhav5@ncsu.edu
Search for other works by this author on:
Prashant Singh,
Prashant Singh
1
Department of Mechanical and Aerospace Engineering,
911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: psingh23@ncsu.edu
North Carolina State University
,911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: psingh23@ncsu.edu
1Corresponding author.
Search for other works by this author on:
Srinath Ekkad
Srinath Ekkad
Department of Mechanical and Aerospace Engineering,
911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: sekkad@ncsu.edu
North Carolina State University
,911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: sekkad@ncsu.edu
Search for other works by this author on:
Srivatsan Madhavan
Department of Mechanical and Aerospace Engineering,
911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: smadhav5@ncsu.edu
North Carolina State University
,911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: smadhav5@ncsu.edu
Prashant Singh
Department of Mechanical and Aerospace Engineering,
911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: psingh23@ncsu.edu
North Carolina State University
,911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: psingh23@ncsu.edu
Srinath Ekkad
Department of Mechanical and Aerospace Engineering,
911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: sekkad@ncsu.edu
North Carolina State University
,911 Oval Dr., Room 3002, Engineering Building III,
Raleigh, NC 27695
e-mail: sekkad@ncsu.edu
1Corresponding author.
Contributed by the Heat Transfer Division of ASME for publication in the Journal of Thermal Science and Engineering Applications. Manuscript received December 18, 2018; final manuscript received April 2, 2019; published online May 22, 2019. Assoc. Editor: Steve Q. Cai.
J. Thermal Sci. Eng. Appl. Dec 2019, 11(6): 061016 (9 pages)
Published Online: May 22, 2019
Article history
Received:
December 18, 2018
Revision Received:
April 2, 2019
Accepted:
April 3, 2019
Citation
Madhavan, S., Singh, P., and Ekkad, S. (May 22, 2019). "Jet Impingement Heat Transfer Enhancement by Packing High-Porosity Thin Metal Foams Between Jet Exit Plane and Target Surface." ASME. J. Thermal Sci. Eng. Appl. December 2019; 11(6): 061016. https://doi.org/10.1115/1.4043470
Download citation file:
Get Email Alerts
Thermal Characteristics and Dryer Performance Analysis of Double Pass Solar Collector Powered by Copper and Iron Oxide
J. Thermal Sci. Eng. Appl (February 2025)
Effect of Variation of the Aspect Ratio of Rectangular Twisted Tapes Inserted in a Circular Pipe on the Thermal Performance
J. Thermal Sci. Eng. Appl (February 2025)
Design Optimization of a Shell-and-Tube Heat Exchanger Based on Variable Baffle Cuts and Sizing
J. Thermal Sci. Eng. Appl (February 2025)
Energy-Efficient Three-Wheel Bleedless Electrical Environmental Control System for a Passenger Aircraft
J. Thermal Sci. Eng. Appl (February 2025)
Related Articles
Integrated Thermal Management System Concept With Combined Jet Plate, High Porosity Aluminum Foam, and Target Plate for Enhanced Heat Transfer
J. Heat Mass Transfer (October,2024)
Direct Simulation of Transport in Open-Cell Metal Foam
J. Heat Transfer (August,2006)
Air Flow Through Compressed and Uncompressed Aluminum Foam: Measurements and Correlations
J. Fluids Eng (September,2006)
Heat Transfer and Pressure Drop of Lotus-Type Porous Metals
J. Heat Transfer (July,2013)
Related Proceedings Papers
Related Chapters
Heat Transfer Enhancement for Thermal Energy Storage Using Metal Foams Embedded within Phase Change Materials (PCMS)
Inaugural US-EU-China Thermophysics Conference-Renewable Energy 2009 (UECTC 2009 Proceedings)
Hydraulic Resistance
Heat Transfer & Hydraulic Resistance at Supercritical Pressures in Power Engineering Applications
Adding Surface While Minimizing Downtime
Heat Exchanger Engineering Techniques