TY - JOUR Y1 - 2024/// A1 - Ahmed, S.W. A1 - Tariq, A. A1 - Altaf, K. A1 - Ali, S. A1 - Hussain, G. A1 - Baharom, M.B. UR - https://www.scopus.com/inward/record.uri?eid=2-s2.0-85188661680&doi=10.1007%2f978-981-99-5946-4_7&partnerID=40&md5=e2b580bb3e3f3e58583ddc0000633150 SN - 21954356 AV - none TI - Thermal Analysis of Helical Pin Fins at Different Pitch Steps Through Numerical Technique N1 - cited By 0; Conference of International Conference on Renewable Energy and E-mobility, ICREEM 2022 ; Conference Date: 1 December 2022 Through 2 December 2022; Conference Code:309409 SP - 71 JF - Lecture Notes in Mechanical Engineering PB - Springer Science and Business Media Deutschland GmbH KW - Fins (heat exchange); Heat convection; Thermoanalysis KW - Comprehensive comparisons; Convection; Convection coefficients; Convective heat transfer; Effective area; Heat transfer rate; Heatsink; Numerical techniques; Optimisations; Pin-fins KW - Computational fluid dynamics N2 - Many modern-day applications rely on heat sinks for heat dissipation. Pin fins are one of the heatsinks that are used for cooling and the convection coefficient of a pin fin depends on many parameters that need optimization. The pin fin in its plain form isn�??t efficient enough and there are ways to not only enhance its heat transfer rate but also reduce its weight simultaneously. This study aims to geometrically modify a plain pin fin to enhance the effective area for convective heat transfer. This study contains a comprehensive comparison between simple pin fin heatsinks and their corresponding heatsinks with helical-shaped profiles on the outer surface. A helical pattern was made using different pitches 2, 4, 6, and 8� mm and they were tested at air speeds of 2, 4, 6 and 8� m/s. Computational fluid dynamic analysis was performed to measure the performance of heatsinks. The tetrahedral mesh was used for simulation, and it was concluded that the helical fin having a 2� mm pitch performed the best and therefore had the highest convection coefficient of 202.69 W/m2K at 8� m/s airspeed. © Institute of Technology PETRONAS Sdn Bhd (Universiti Teknologi PETRONAS) 2024. EP - 83 ID - scholars20116 ER -