eprintid: 11231 rev_number: 2 eprint_status: archive userid: 1 dir: disk0/00/01/12/31 datestamp: 2023-11-10 03:25:45 lastmod: 2023-11-10 03:25:45 status_changed: 2023-11-10 01:14:46 type: article metadata_visibility: show creators_name: Tariq, A. creators_name: Altaf, K. creators_name: Rani, A.M.A. creators_name: Baharom, M. creators_name: Aziz, A.R.A. title: Study of heat transfer attributes of custom fins for Crank-Rocker engine block using ANSYS ispublished: pub note: cited By 6 abstract: Crank-rocker engine (CRE) is an internal combustion (IC) engine with a curved piston and cylinder, developed at Universiti Teknologi PETRONAS (UTP) Malaysia. Heat is generated during combustion in an IC engine, some portion of which is converted into the mechanical energy. Almost 30 of the generated heat needs to be dissipated through engine walls. Fins are used to provide additional surface area to engine block for dissipation of excess heat. Transient thermal analysis of existing 3-fins model of CRE is performed at different engine speeds, using 'ANSYS Transient Thermal' module. With the understanding of thermal behavior of the existing 3-fins model, new straight and curved conformal fin models, with increased surface area and better fin effectiveness, are proposed. Thermal performance of both, straight and curved fin models, is compared with existing 3-fins model of crank-rocker engine. © 2019 PENERBIT AKADEMIA BARU. date: 2019 publisher: Penerbit Akademia Baru official_url: https://www.scopus.com/inward/record.uri?eid=2-s2.0-85075816068&partnerID=40&md5=8d504cb50fc2635408e3c2452ef99648 full_text_status: none publication: Journal of Advanced Research in Fluid Mechanics and Thermal Sciences volume: 62 number: 2 pagerange: 235-243 refereed: TRUE issn: 22897879 citation: Tariq, A. and Altaf, K. and Rani, A.M.A. and Baharom, M. and Aziz, A.R.A. (2019) Study of heat transfer attributes of custom fins for Crank-Rocker engine block using ANSYS. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 62 (2). pp. 235-243. ISSN 22897879