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NACA Airfoils as Proposal for Heat Sink Fins: Optimization Investigation

J. Luis Luviano-Ortiz, Julio Cesar Rodriguez-Mosqueda, Salvador Botello-Aceves, Yanan Camaraza-Medina*, Abel Hernandez-Guerrero

Department of Mechanical Engineering, University of Guanajuato, Salamanca, 36787, Mexico

* Corresponding Author: Yanan Camaraza-Medina. Email: email

(This article belongs to the Special Issue: Advances in Heat and Mass Transfer: Integrating Numerical Methods with Artificial Intelligence, Machine Learning, and Data-Driven Approaches)

Frontiers in Heat and Mass Transfer 2025, 23(4), 1165-1183. https://doi.org/10.32604/fhmt.2025.067466

Abstract

This work presents a simulation analysis using a multi-objective evolutionary algorithm for the thermo-hydraulic behavior of staggered heat sinks whose fins have NACA 0040 airfoil profile. The results were compared with a conventional pin fin heat sink with a circular profile. This study searched for the best thermo-hydraulic performance by translational and rotational positioning of the fins. It is worth mentioning that this work was carried out in two stages. In the first stage, the thermo-hydraulic behavior of the heat sink was studied moving the location of the upper array above the X-axis from −2.25 to 2.25 mm and above the Y-axis from −1.55 to 1.275 mm. The second stage examined the effects of fin rotation considering the results found in stage 1. However, in this second stage, both arrays were free to rotate. For the upper array, the rotation range was −25° to 25° and for the lower array the rotation range was −15° to 15°. It is worth mentioning that both stages were analyzed for a single Reynolds (Re) number value of 13,000. The optimization results using the multi-objective evolutionary algorithm showed that compared to a NACA 0040 heat sink with fixed, unrotated original configuration (C0), the NACA 0040 heat sink with any Position Configuration (PC) did not significantly improve the heat transfer. Then, the results found in the second stage showed that the effect of the rotation of both sets did not influence the increase in pressure drop. However, it was found that with the Optimal Position and Rotation Configuration (PRCoptimal), which is the optimized array from Stage 1 (position) then optimized by rotation, there is a slightly higher Performance Evaluation Criterion (PEC) compared to the original C0 configuration by 7%. Finally, the proposed NACA 0040 heat sink with the optimal rotation and position setting (PRCoptimal) was found to have a PEC of 9% compared to a conventional pin fin heat sink.

Keywords

NACA airfoil; fins; optimization; simulation; multiphysics; performance evaluation criterion (PEC)

Cite This Article

APA Style
Luviano-Ortiz, J.L., Rodriguez-Mosqueda, J.C., Botello-Aceves, S., Camaraza-Medina, Y., Hernandez-Guerrero, A. (2025). NACA Airfoils as Proposal for Heat Sink Fins: Optimization Investigation. Frontiers in Heat and Mass Transfer, 23(4), 1165–1183. https://doi.org/10.32604/fhmt.2025.067466
Vancouver Style
Luviano-Ortiz JL, Rodriguez-Mosqueda JC, Botello-Aceves S, Camaraza-Medina Y, Hernandez-Guerrero A. NACA Airfoils as Proposal for Heat Sink Fins: Optimization Investigation. Front Heat Mass Transf. 2025;23(4):1165–1183. https://doi.org/10.32604/fhmt.2025.067466
IEEE Style
J. L. Luviano-Ortiz, J. C. Rodriguez-Mosqueda, S. Botello-Aceves, Y. Camaraza-Medina, and A. Hernandez-Guerrero, “NACA Airfoils as Proposal for Heat Sink Fins: Optimization Investigation,” Front. Heat Mass Transf., vol. 23, no. 4, pp. 1165–1183, 2025. https://doi.org/10.32604/fhmt.2025.067466



cc Copyright © 2025 The Author(s). Published by Tech Science Press.
This work is licensed under a Creative Commons Attribution 4.0 International License , which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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