Graduation Semester and Year
2024
Language
English
Document Type
Thesis
Degree Name
Master of Science in Aerospace Engineering
Department
Mechanical and Aerospace Engineering
First Advisor
Dereje Agonafer
Abstract
In 1965, Intel co-founder Gordon Moore made the observation that the transistor counts on a chip double with a frequency of approximately every two years. This development resulted in more compact and potent ICs. However, the amount of heat produced on a chip increased proportionally with the number of transistors. Later, in the early 2000s, Dennard Scaling broke down. Transistors became so small that leakage currents (unwanted currents that flow within the transistor) emerged as a significant issue, and they contributed substantially to power consumption and heat generation. These tightly packed transistors produced heat, which decreased their performance and shortened their lifespan, as well as causing the IC to fail. As a result, efficient cooling systems became increasingly crucial in electronics, particularly in high-performance computing, to dissipate this heat and maintain the reliability and performance of the devices. Advanced cooling techniques, such as liquid cooling, phase-change cooling, and advanced materials for heat dissipation, are widely used. Single-phase liquid immersion cooling is a method of cooling electronic components where the components are completely immersed in a dielectric liquid (electrically non-conductive). In conditions where high-performance computing and data center applications require significant heat dissipation, single-phase liquid immersion cooling is a more efficient technique than air cooling, particularly in high heat flux, efficient heat removal, uniform cooling, improved reliability, and longevity of components. The process is termed "single-phase" because the cooling liquid remains in the same phase. This work presents an experimental study on the thermal performance of aluminum foam heat sinks in single-phase liquid immersion cooling (SPLIC). A set of heat sinks with varying pores per inch (PPI) and height is employed to test the thermal properties of heat sinks under different flow rates and power. Metal foams are used in place of conventional heat sinks for cooling, particularly aluminum alloy (Al-6101-T6) foam, which is a type of lightweight porous material with a cellular structure consisting of a large volume fraction of gas-filled open pores. It has a higher surface area-to-volume ratio, higher thermal conductivity, is lightweight, has increased turbulence, and has structural integrity at high temperatures. The goal of this experiment is to analyze the thermal and fluid properties of an aluminum foam heat sink when it is immersed in a synthetic dielectric fluid (EC-100). A customized tank was designed and fabricated for the experimental setup with a Thermal Test Vehicle (TTV), enabling the control of flow rate, heater temperature, and inlet temperature of the fluid. A set of experiments were conducted using aluminum foam heat sinks with varying pores per inch (5, 10, 20, and 40 PPI) for varying flow rates (1, 2, and 3 LPM) and heights (0.5 and 0.75 inches) with a relative density of 10~12%, mounted on a heater plate with heat fluxes of 19 W/cm^2 and 23.8 W/cm^2 respectively. Major outcomes from the experiment were that the heat sink of 10 PPI exhibited the best heat transfer and lowest thermal resistance, while the heat sink of 5 PPI exhibited the highest “overall surface area efficiency” in all conditions. The heat transfer was increased from 0.5-inch-high to 0.75-inch-hight foam cores.
Keywords
SPLIC) single-phase liquid immersion cooling, Heat flux, Pores per inch (PPI), Heat transfer, Forced convection, Data center, Metal foam
Disciplines
Aerospace Engineering | Engineering | Mechanical Engineering
License
This work is licensed under a Creative Commons Attribution-NonCommercial-Share Alike 4.0 International License.
Recommended Citation
Kumawat, Manish, "EXPERIMENTAL STUDY ON THERMAL PERFORMANCE OF METAL FOAM HEAT SINKS IN SINGLE PHASE LIQUID IMMERSION COOLING" (2024). Mechanical and Aerospace Engineering Theses. 1019.
https://mavmatrix.uta.edu/mechaerospace_theses/1019
Comments
Degree granted by The University of Texas at Arlington