Study of the aerodynamic structure around a NACA6409 Aairfoil rotor

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dc.contributor.authorGouiaa, Saoussane
dc.contributor.authorAmeni, Ameni
dc.contributor.authorDriss, Zied
dc.contributor.authorBen Amira, Bilel
dc.date.accessioned2023-04-30T10:50:00Z
dc.date.available2023-04-30T10:50:00Z
dc.date.issued2017-04-11
dc.descriptionArticleen_US
dc.description.abstractThe multi-copters are one of the important aircrafts in the world because they are used in both military and civil application. The problem of these aircrafts is the low efficiency of its propellers. That’s why, it is necessary to study the aerodynamic structure around every rotor. In this paper, a computer simulation has been done to study the aerodynamic structure around a NACA 6409 airfoil rotor. The numerical model is based on the resolution of the Navier - Stockes equations with a standard k-ε model. Then, the finite volume discretization of these equations leads to solve it. The local characteristics of the aerodynamic structure are extracted using the software Solidworks Flow Simulation and the validation is done with comparison with anterior result of Alexandrov [1].en_US
dc.identifier.citationGouiaa ,Saoussane. Mehdi, Ameni. Zied ,Driss. Bilel, Ben Amira, Mohamed Salah Abid. Study of the aerodynamic structure around a NACA6409Aairfoil rotor. International Journal of Energetica. Vo2. No 01.11/04/2017.faculty of technology. university of el oued. [visited in ../../….]. available from [copy the link here]en_US
dc.identifier.issn2543-3717
dc.identifier.urihttp://dspace.univ-eloued.dz/handle/123456789/21002
dc.language.isoenen_US
dc.publisherجامعة الوادي - university of el oueden_US
dc.subjectNACA 6409 airfoil rotor, aerodynamic structure, computer simulation, CFDen_US
dc.titleStudy of the aerodynamic structure around a NACA6409 Aairfoil rotoren_US
dc.typeArticleen_US

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