- All Journals
- Al-Qadisiyah University
- Basrah University
- Kirkuk University
- Mosul University
- The Iraqi Borad for Medical Specialization
- University of Anbar
- University of Technology
- Al Mustafa University
- Al-Zahraa University for Women
- Alnoor University
- Kunooz University
- Misan University
- Ninevah University
- Tikrit University
- University of Al-Hamdaniya
- University of Kerbala
NUMERICAL SOLUTIONS FOR POTENTIAL FLOW PASTS 2 – D LIFTING AIRFOILS | ||
| Al-Qadisiyah Journal for Engineering Sciences | ||
| Article 1, Volume 1, Issue 2, 2008, Pages 180-187 PDF (0 K) | ||
| Author | ||
| Hayder Aziz Neema | ||
| Abstract | ||
| 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. | ||
|
Statistics Article View: 169 PDF Download: 130 |
||