A triangle space with a submerged cold cylinder of varying sizes and shapes is the subject of this computational investigation of spontaneous thermal convection. The (Al2O3-Cuwater) hybrid nanofluid fills the triangle space using an aspect ratio and the geometry of the cold source immersed in the solar panel. The objective of this project is to enhance the performance of the panel by increasing the evacuation rate of convective heat transfer. The second goal is to conduct digital research that will enable a reliable selection of data for the panel future design. Therefore, this work has significance since it allows for lowering the temperature and boosting the solar panel efficiency despite the challenging conditions in our dry border region (southwest Algeria). With a Rayleigh number of 106 and based on information from our dry location (southwest Algeria), with the solar panel angled at 30°, we tested three distinct cases: one with SL=0.04, another with SL=0.06 and the last one with SL= 0.08. The coupling of the flow governing equations in our investigation is solved by a quadratic Lagrange interpolation utilizing the finite element approach. Following the establishment of the optimal dimension, five distinct shapes of the cold source are examined to ascertain the best shape for the evacuation of convective heat transfer within a triangle cavity. Temperature profiles, average Nusselt number, streamline and isotherm patterns are all part of the collected data. Based on the findings of this experiment, the convective transfer mode can only be dominant when the source is circular with a diameter of SL= 0.08. Near the source, it has been found that the temperature of the solar panel is reduced, which is a significant result. There is a strong agreement when we compare the average Nusselt number of our code to that of Keramat.
Hybrid Nanofluid Circular Cold Cylinder Square Cold Cylinder Temperature Solar Panel Natural Convection FiniteElement Method Triangular Cavity
Primary Language | English |
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Subjects | Aerodynamics (Excl. Hypersonic Aerodynamics) |
Journal Section | Articles |
Authors | |
Publication Date | July 31, 2025 |
Submission Date | May 23, 2024 |
Acceptance Date | August 24, 2024 |
Published in Issue | Year 2025 Volume: 11 Issue: 4 |
IMPORTANT NOTE: JOURNAL SUBMISSION LINK http://eds.yildiz.edu.tr/journal-of-thermal-engineering