Thermal-hydraulic modeling of heat sink under force convection: Investigating the effect of wings on new designs
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F23%3A00373579" target="_blank" >RIV/68407700:21220/23:00373579 - isvavai.cz</a>
Výsledek na webu
<a href="https://doi.org/10.1016/j.aej.2022.10.045" target="_blank" >https://doi.org/10.1016/j.aej.2022.10.045</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1016/j.aej.2022.10.045" target="_blank" >10.1016/j.aej.2022.10.045</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Thermal-hydraulic modeling of heat sink under force convection: Investigating the effect of wings on new designs
Popis výsledku v původním jazyce
This study aims to investigate the heat transfer performance and fluid flow characteristics of different geometrical configurations of new heat sinks. The effect of wings and number of pins on the performance of the heat sinks were numerically investigated. Rigorous heat transfer models, including its associated physical parameters such as surface area were derived for each new design. The results show that adding wings to the pin fins significantly increases heat dissipation from the hot spots. However, there was 47 % heat transfer enhancement of Perforated Hollow Pin-Fin Heat Sink (PHPFHS) with wings when compared with (PHPFHS) without wings. At a velocity of 5 m/s, the corresponding pressure drop for Cone Pin-Fin Heat Sink (CPFHS) without Wings is 10 Pa and that of CPFHS with wings is about 23 Pa. The formation of vortex at the rear of the pin fins causes an increase in pressure drop. The CPFHS with wings has the maximum thermal performance index g which ranges from 1.6 to 2.4 The complex structure of the heat sinks with wings increases the flow resistance and suppresses the flow separation. A relative comparison of the results shows that vortex formation is minimal and suppressed for heat sinks without wings.
Název v anglickém jazyce
Thermal-hydraulic modeling of heat sink under force convection: Investigating the effect of wings on new designs
Popis výsledku anglicky
This study aims to investigate the heat transfer performance and fluid flow characteristics of different geometrical configurations of new heat sinks. The effect of wings and number of pins on the performance of the heat sinks were numerically investigated. Rigorous heat transfer models, including its associated physical parameters such as surface area were derived for each new design. The results show that adding wings to the pin fins significantly increases heat dissipation from the hot spots. However, there was 47 % heat transfer enhancement of Perforated Hollow Pin-Fin Heat Sink (PHPFHS) with wings when compared with (PHPFHS) without wings. At a velocity of 5 m/s, the corresponding pressure drop for Cone Pin-Fin Heat Sink (CPFHS) without Wings is 10 Pa and that of CPFHS with wings is about 23 Pa. The formation of vortex at the rear of the pin fins causes an increase in pressure drop. The CPFHS with wings has the maximum thermal performance index g which ranges from 1.6 to 2.4 The complex structure of the heat sinks with wings increases the flow resistance and suppresses the flow separation. A relative comparison of the results shows that vortex formation is minimal and suppressed for heat sinks without wings.
Klasifikace
Druh
J<sub>imp</sub> - Článek v periodiku v databázi Web of Science
CEP obor
—
OECD FORD obor
20303 - Thermodynamics
Návaznosti výsledku
Projekt
—
Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2023
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
AEJ - Alexandria Engineering Journal
ISSN
1110-0168
e-ISSN
2090-2670
Svazek periodika
65
Číslo periodika v rámci svazku
2
Stát vydavatele periodika
AT - Rakouská republika
Počet stran výsledku
22
Strana od-do
709-730
Kód UT WoS článku
000920750200001
EID výsledku v databázi Scopus
2-s2.0-85140981158