INDIRECT PANEL METHOD FOR IDEAL FLOW AROUND A SYMMETRIC AEROFOIL WITH CONSTANT VARIATION

Authors

  • M. Mushtaq 1Department of Mathematics, U.E.T. Lahore – Pakistan.

DOI:

https://doi.org/10.57041/pjs.v65i3.590

Keywords:

Indirect Panel Method, Ideal Flow, Symmetric Aerofoil, Constant Variation.

Abstract

In this paper, the indirect panel method is used to compute the velocity distribution over the surface of a symmetric aerofoil 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 surface of a symmetric aerofoil.

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Published

2022-12-28

How to Cite

M. Mushtaq. (2022). INDIRECT PANEL METHOD FOR IDEAL FLOW AROUND A SYMMETRIC AEROFOIL WITH CONSTANT VARIATION. Pakistan Journal of Science, 65(3). https://doi.org/10.57041/pjs.v65i3.590

Issue

Vol. 65 No. 3 (2013): Pakistan Journal of Science

Section

Articles

License

Copyright (c) 2013 Pakistan Journal of Science

Creative Commons License

This work is licensed under a Creative Commons Attribution-ShareAlike 4.0 International License.

http://creativecommons.org/licenses/by-sa/4.0