Aerodynamic analysis of DLR–F4 model using panel method. | [Proc 3rd Int Bhurban Conf Appl Sci Technol • 2003]

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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