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.
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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Ahmed Soliman M.Sherif. 2017. “. Global Journal of Research in Engineering – A : Mechanical & Mechanics GJRE-A Volume 17 (GJRE Volume 17 Issue A2): .
Crossref Journal DOI 10.17406/gjre
Print ISSN 0975-5861
e-ISSN 2249-4596
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