Numerical Simulation Andmodelingofunsteady Flowaround Anairfoil. (aerodynamic Form)
| dc.contributor.author | Habib, M. Y. | |
| dc.contributor.author | Djaaffar, R. | |
| dc.date.accessioned | 2020-10-21T08:16:08Z | |
| dc.date.available | 2020-10-21T08:16:08Z | |
| dc.date.issued | 2014-01-01 | |
| dc.description | Articale in Journal of fundamental and Applied Sciences Vol. 06 N. 01 | en_US |
| dc.description.abstract | Duringthis work, we simulatedanunsteady flowaround anairfoiltypeNACA0012using theFluent software. The objectiveis to controlthe codeon the one handandon the other handthe simulationofunsteady flows. By simulatinganunsteady flowReynolds number(Re =6.85*106) andMach number(M =0.3), we havethe flowingwitha grid(mesh) adequatenumerical resultsandexperimental dataare ingood agreement. To representthe results ofthe simulationwe havevalidated bycomparing the valuesof aerodynamic coefficientswith those ofexperimental data. | en_US |
| dc.identifier.citation | Articale in Journal of fundamental and Applied Sciences Vol. 06 N. 01 | en_US |
| dc.identifier.issn | 1112-9867 | |
| dc.identifier.uri | http://dspace.univ-eloued.dz/handle/123456789/7203 | |
| dc.language.iso | en | en_US |
| dc.publisher | University of Eloued جامعة الوادي | en_US |
| dc.subject | Unsteady flow; Fluent;a singleequationmodel;NACA0012. | en_US |
| dc.title | Numerical Simulation Andmodelingofunsteady Flowaround Anairfoil. (aerodynamic Form) | en_US |
| dc.type | Article | en_US |
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