No Detail Found!

Aerodynamic analysis of DLR–F4 model using panel method.

Author(s)
Asif Mushtaq National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
Farhan Abbas National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
M. Asif National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
S. Zahir National Engineering and Scientific Commission (NESCOM), Islamabad, Pakistan
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%.
Publication Details
Page(s) 343-351
DOI DOI not available
Published Journal: Proc 3rd Int Bhurban Conf Appl Sci Technol, Volume: 0, Issue: 0, Year: 2003

Request the full text from PASTIC

More from Proc 3rd Int Bhurban Conf Appl Sci Technol
0

Citations

0

Downloads

96

Views

Copyright ©  PASTIC National Center, Islamabad www.pastic.gov.pk