Numerical Simulation Andmodelingofunsteady Flowaround Anairfoil. (aerodynamic Form)
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Date
2014-01-01
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University of Eloued جامعة الوادي
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.
Description
Articale in Journal of fundamental and Applied Sciences Vol. 06 N. 01
Keywords
Unsteady flow; Fluent;a singleequationmodel;NACA0012.
Citation
Articale in Journal of fundamental and Applied Sciences Vol. 06 N. 01