INDIRECT BOUNDARY INTEGRAL EQUATION METHOD FOR SUBSONIC FLOW AROUND JOUKOWSKI AEROFOIL USING SOURCE DISTRIBUTION ALONE

Authors

  • Muhammad Mushtaq uet. lahore
  • Haseeb Muzaffar uet,LAHOR
  • Ghulam Muhammad deptt. of math. GCS, Wahdat Road, LAhore
  • Muhammad Arif Khan UET, Lahore
  • Sabahat Arif Khan UET, lahor
  • yasir nadeem anjam

Keywords:

Indirect boundary integral equation method, subsonic flow, Joukowski aerofoil.

Abstract

In this paper, the indirect boundary integral equation method is used to compute the subsonic flow (i.e. velocity distribution) over the boundary of a Joukowski aerofoil using source distribution alone for which the exact result is present. To check the accuracy of the method; the computed flow velocity is compared to the exact result for the flow over the boundary of a joukowski aerofoil.

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Published

2013-08-06

How to Cite

Mushtaq, M., Muzaffar, H., Muhammad, G., Khan, M. A., Khan, S. A., & anjam, yasir nadeem. (2013). INDIRECT BOUNDARY INTEGRAL EQUATION METHOD FOR SUBSONIC FLOW AROUND JOUKOWSKI AEROFOIL USING SOURCE DISTRIBUTION ALONE. Journal of the Pakistan Institute of Chemical Engineers, 41(1), 21–31. Retrieved from http://piche.org.pk/journal/index.php/jpiche/article/view/99

Issue

Vol. 41 No. 1 (2013): Journal of the Pakistan Institute of Chemical Engineers

Section

Articles

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