@article{(Open Science Index):https://publications.waset.org/pdf/14806,
	  title     = {Aerodynamic Stall Control of a Generic Airfoil using Synthetic Jet Actuator},
	  author    = {Basharat Ali Haider and  Naveed Durrani and  Nadeem Aizud and  Salimuddin Zahir},
	  country	= {},
	  institution	= {},
	  abstract     = {The aerodynamic stall control of a baseline 13-percent
thick NASA GA(W)-2 airfoil using a synthetic jet actuator (SJA) is
presented in this paper. Unsteady Reynolds-averaged Navier-Stokes
equations are solved on a hybrid grid using a commercial software to
simulate the effects of a synthetic jet actuator located at 13% of the
chord from the leading edge at a Reynolds number Re = 2.1x106 and
incidence angles from 16 to 22 degrees. The experimental data for the
pressure distribution at Re = 3x106 and aerodynamic coefficients at
Re = 2.1x106 (angle of attack varied from -16 to 22 degrees) without
SJA is compared with the computational fluid dynamic (CFD)
simulation as a baseline validation. A good agreement of the CFD
simulations is obtained for aerodynamic coefficients and pressure
distribution.
A working SJA has been integrated with the baseline airfoil and
initial focus is on the aerodynamic stall control at angles of attack
from 16 to 22 degrees. The results show a noticeable improvement in
the aerodynamic performance with increase in lift and decrease in
drag at these post stall regimes.},
	    journal   = {International Journal of Aerospace and Mechanical Engineering},
	  volume    = {4},
	  number    = {9},
	  year      = {2010},
	  pages     = {788 - 793},
	  ee        = {https://publications.waset.org/pdf/14806},
	  url   	= {https://publications.waset.org/vol/45},
	  bibsource = {https://publications.waset.org/},
	  issn  	= {eISSN: 1307-6892},
	  publisher = {World Academy of Science, Engineering and Technology},
	  index 	= {Open Science Index 45, 2010},
	}