@article{(Open Science Index):https://publications.waset.org/pdf/9998176,
	  title     = {Large Eddy Simulation of Flow Separation Control over a NACA2415 Airfoil},
	  author    = {M. Tahar Bouzaher},
	  country	= {},
	  institution	= {},
	  abstract     = {This study involves a numerical simulation of the flow around a NACA2415 airfoil, with a 15°angle of attack, and flow separation control using a rod, It reposes inputting a cylindrical rod upstream of the leading edge in order to accelerate the transition of the boundary layer by interaction between the rod wake and the boundary layer. The viscous, non-stationary flow is simulated using ANSYS FLUENT 13. Our results showed a substantial modification in the flow behavior and a maximum drag reduction of 51%.
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {8},
	  number    = {5},
	  year      = {2014},
	  pages     = {880 - 883},
	  ee        = {https://publications.waset.org/pdf/9998176},
	  url   	= {https://publications.waset.org/vol/89},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 89, 2014},