The Effect of Supersonic Flows on Different Profiles of Aircraft Wings
Keywords:
CAE, frequencies, dynamic, stress, deformation, CNC
Abstract
When a supersonic stream flows around a thin profile, the pressure acting on the surface element does not depend on the shape of the rest of the profile, but depends only on the slope of the element itself, that is, on the local angle of attack. The local angle of attack is the angle between the surface element and the velocity vector of the undisturbed flow Coefficient of pressure.
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How to Cite
Ahmed Soliman M.Sherif. (2017). The Effect of Supersonic Flows on Different Profiles of Aircraft Wings. Global Journals of Research in Engineering, 17(A2), 9–26. Retrieved from https://engineeringresearch.org/index.php/GJRE/article/view/1561
Published
2017-01-15
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Copyright (c) 2017 Authors and Global Journals Private Limited
This work is licensed under a Creative Commons Attribution 4.0 International License.