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dc.contributor.authorGabbasa, Asya A.
dc.contributor.authorAssaleh, Tarak
dc.contributor.authorDabbashi, Siddig
dc.date.accessioned2020-11-23T23:02:53Z
dc.date.available2020-11-23T23:02:53Z
dc.date.issued2019-05
dc.identifier.issn2519-674X
dc.identifier.urihttp://dspace.zu.edu.ly/xmlui/handle/1/939
dc.description.abstractComputation fluid dynamics (CFD) simulations are very important tools, which use algorithms and numerical methods for analyzing and solving problems in fluid mechanics. Computer programs are adopted in order to simulate the interaction between gases and liquids with boundary conditions. The programs have the ability to undertake speedy and accurate simulations of complex scenarios, which include turbulent and transonic flows. This paper aims to study an incompressible, viscous, turbulent flow over multi-element airfoils. The governing equations (NS) are solved by using k-epsilon model and SIMPLE algorithm turbulent, steady-state, incompressible flow using the commercial code ANSYS Fluent. Detailed studies are done at different angle of attack flight conditions. By using kepsilon model and simple algorithm we have obtained the accurate results; that is successful in comparing with wind tunnel results of NACA23012en_US
dc.language.isoenen_US
dc.subjectFluid mechanics, Naiver-Stokes equations, viscous fluid flowen_US
dc.titleValidation Solution of Incompressible Viscous Flow Over Multi-Element Airfoilen_US
dc.typeArticleen_US


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  • Vol.3- المجلد الثالث [12]
    حولية علمية محكمة تصدر عن مركز البحوث والاستشارات العلمية والتدريب بجامعة الزاوية

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