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Aerodynamic analysis of DLR–F4 model using panel method.
Author(s):
1. Asif Mushtaq: National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
2. Farhan Abbas: National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
3. M. Asif: National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
4. S. Zahir: National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
5. M. A. Khan: National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
Abstract:
Aerodynamic analysis of DLR-F4 Wing-Body configuration has been done, using Panel Method. Aerodynamic response of the model has been investigated and results are compared with the Wind Tunnel data [1]. Lift, Drag and Pitching-moment coefficients have been calculated. It has been found that results are comparable with that obtained by Wind Tunnel and the variation is within ± 10%.
Page(s): 343-351
DOI: DOI not available
Published: Journal: Proc 3rd Int Bhurban Conf Appl Sci Technol, Volume: 0, Issue: 0, Year: 2003
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