A multi-objective and CFD based optimization of roof-flap geometry and position for simultaneous drag and lift reduction

dc.authoridBaghoolizadeh, Mohammadreza/0000-0002-3703-0866
dc.authoridRostamzadeh-Renani, Mohammad/0000-0003-4744-5499
dc.authorscopusid57216954326
dc.authorscopusid57338920800
dc.authorscopusid22136195900
dc.authorscopusid57216950040
dc.authorscopusid58126363400
dc.authorscopusid23028598900
dc.authorscopusid23028598900
dc.contributor.authorRostamzadeh-Renani, Mohammad
dc.contributor.authorSalahshour, Soheıl
dc.contributor.authorSajadi, S. Mohammad
dc.contributor.authorRostamzadeh-Renani, Reza
dc.contributor.authorAzarkhavarani, Narjes Khabazian
dc.contributor.authorSalahshour, Soheil
dc.contributor.authorToghraie, Davood
dc.date.accessioned2024-05-25T12:18:49Z
dc.date.available2024-05-25T12:18:49Z
dc.date.issued2024
dc.departmentOkan Universityen_US
dc.department-temp[Rostamzadeh-Renani, Mohammad; Rostamzadeh-Renani, Reza] Politecn Milan, Energy Dept, Via Lambruschini 4, I-20156 Milan, Italy; [Baghoolizadeh, Mohammadreza] Shahrekord Univ, Dept Mech Engn, Shahrekord 8818634141, Iran; [Sajadi, S. Mohammad] Cihan Univ Erbil, Dept Nutr, Erbil, Kurdistan Reg, Iraq; [Azarkhavarani, Narjes Khabazian] Jami Inst Technol, Dept Mech Engn, Esfahan, Iran; [Salahshour, Soheil] Istanbul Okan Univ, Fac Engn & Nat Sci, Istanbul, Turkiye; [Salahshour, Soheil] Bahcesehir Univ, Fac Engn & Nat Sci, Istanbul, Turkiye; [Salahshour, Soheil] Lebanese Amer Univ, Dept Comp Sci & Math, Beirut, Lebanon; [Toghraie, Davood] Islamic Azad Univ, Dept Mech Engn, Khomeinishahr Branch, Khomeinishahr, Iranen_US
dc.descriptionBaghoolizadeh, Mohammadreza/0000-0002-3703-0866; Rostamzadeh-Renani, Mohammad/0000-0003-4744-5499en_US
dc.description.abstractAs the transport sector is responsible for the consumption of a vast proportion of the oil produced, it is mandatory to research feasible solutions to tackle this issue. The application of aerodynamic attachments for passive flow control and reducing resisting aerodynamic forces such as drag and lift is one of the most practicable ways to minimize vehicle energy consumption. The flaps are one of the most innovative aerodynamic attachments that can enhance the flow motion in the boundary layer at the trailing edge of the wings. In the present paper, the flap is designed and modeled for controlling the airflow at the roof-end of a 2D Ahmed body model, inspired by the schematic of the flap at the trailing edge of the wing. As a result, the flap 's geometry and position from the roof -end of the car model are parameterized, which leads to having four design variables. The objective functions of the present study are the vehicle 's drag coefficient and lift coefficient. 25 Design of Experiment (DOE) points are considered enabling the Box-Behnken method. Then, each DOE point is modeled in the computational domain, and the flow -field around the model is simulated using Ansys Fluent software. The results obtained for the DOE points are employed by different regressors, and the relation between design variables and objective functions is extracted using GMDH-ANN. The GMDH-ANN is then coupled with three types of optimization algorithms, among which the Genetic algorithm proves to have the most ideal coupling process for optimization. Finally, after analyzing the variations in the geometry and position of the roof flap from the car roof -end, the roof -flap with specifications of L = 0.1726 m, a = 5.0875 degrees , H = 0.0188 m, and d = 0.241 m can optimize the car drag and lift coefficients by 21.27% and 19.91%, respectively. The present research discusses the opportunities and challenges of optimal design roof -flap geometry and its influence on car aerodynamic performance. <feminine ordinal indicator> 2024 The Authors. Publishing services by Elsevier B.V. on behalf of KeAi Communications Co. Ltd. This is an open access article under the CC BY -NC -ND license (http://creativecommons.org/licenses/bync-nd/4.0/).en_US
dc.description.woscitationindexScience Citation Index Expanded
dc.identifier.citation3
dc.identifier.doi10.1016/j.jppr.2024.02.004
dc.identifier.endpage45en_US
dc.identifier.issn2212-540X
dc.identifier.issue1en_US
dc.identifier.scopus2-s2.0-85187994754
dc.identifier.scopusqualityQ1
dc.identifier.startpage26en_US
dc.identifier.urihttps://doi.org/10.1016/j.jppr.2024.02.004
dc.identifier.volume13en_US
dc.identifier.wosWOS:001222645800001
dc.identifier.wosqualityQ1
dc.institutionauthorSalahshour S.
dc.language.isoen
dc.publisherKeai Publishing Ltden_US
dc.relation.ispartofPropulsion and Power Researchen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectDrag coef fi cienten_US
dc.subjectLift coef fi cienten_US
dc.subjectRoof fl apen_US
dc.subjectComputational fl uid dynamicsen_US
dc.subjectArti fi cial neuralen_US
dc.subjectnetworken_US
dc.subjectGenetic algorithmen_US
dc.titleA multi-objective and CFD based optimization of roof-flap geometry and position for simultaneous drag and lift reductionen_US
dc.typeArticleen_US
dspace.entity.typePublication
relation.isAuthorOfPublicationf5ba517c-75fb-4260-af62-01c5f5912f3d
relation.isAuthorOfPublication.latestForDiscoveryf5ba517c-75fb-4260-af62-01c5f5912f3d

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