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Performance assessment of the vortex panel method

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dc.contributor.author Sultan, Khalid M
dc.contributor.author Elshabli, Anas M
dc.contributor.author Kashbour, Mohammed A
dc.contributor.author Ben.Ateiga, Seraj A
dc.date.accessioned 2020-10-07T12:08:37Z
dc.date.available 2020-10-07T12:08:37Z
dc.date.issued 2019-06-15
dc.identifier.issn 2663-1407
dc.identifier.uri http://repository.uob.edu.ly/handle/123456789/1318
dc.description.abstract The vortex panel method is a very simple and computationally effective method to solve the incompressible and inviscid flow past thin airfoils. This work tries to provide a complete and detailed presentation of the mathematical derivation of this method. It also highlights the points of strength and weakness of this method as compared with more advanced yet expensive computational methods. The results obtained from this work have shown that the method is capable of solving the flow past thin airfoils with good precision for subsonic and laminar flow. For transonic and turbulent flows and as the angle of attack of the flow is increased, the method lacks the precision, especially near the leading and trailing edges. en_US
dc.language.iso en en_US
dc.publisher Universty of Benghazi en_US
dc.relation.ispartofseries Volume 9, Number 2;
dc.subject Vortex panel method en_US
dc.subject Potential flow solutions en_US
dc.subject Kutta condition en_US
dc.subject CFX en_US
dc.subject Matlab en_US
dc.title Performance assessment of the vortex panel method en_US
dc.type Working Paper en_US

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