The ability of the panel methods in solving the potential flow problem around 2-D lifting airfoils is tested in this study. The approximate solutions for potential flow pasts thick, thin, symmetrical, and non-symmetrical airfoils have been calculated by using panel methods and then compared with either the exact analytical solution or the numerical solution obtained by using a perturbation method. As a results, the linear-varying strength vortex method is seemed to be the better one in precision in solving the all four problems.
Aziz Neema,H . (2008). NUMERICAL SOLUTIONS FOR POTENTIAL FLOW PASTS 2 – D LIFTING AIRFOILS. Al-Qadisiyah Journal for Engineering Sciences, 1(2), 180-187.
MLA
Aziz Neema,H . "NUMERICAL SOLUTIONS FOR POTENTIAL FLOW PASTS 2 – D LIFTING AIRFOILS", Al-Qadisiyah Journal for Engineering Sciences, 1, 2, 2008, 180-187.
HARVARD
Aziz Neema H. (2008). 'NUMERICAL SOLUTIONS FOR POTENTIAL FLOW PASTS 2 – D LIFTING AIRFOILS', Al-Qadisiyah Journal for Engineering Sciences, 1(2), pp. 180-187.
CHICAGO
H Aziz Neema, "NUMERICAL SOLUTIONS FOR POTENTIAL FLOW PASTS 2 – D LIFTING AIRFOILS," Al-Qadisiyah Journal for Engineering Sciences, 1 2 (2008): 180-187,
VANCOUVER
Aziz Neema H. NUMERICAL SOLUTIONS FOR POTENTIAL FLOW PASTS 2 – D LIFTING AIRFOILS. QJES. 2008;1(2):180-187.
