ALGEBRAIC PREDICTION OF TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT | ||||
International Conference on Aerospace Sciences and Aviation Technology | ||||
Article 5, Volume 1, A.S.A.T. CONFERENCE 14-16 May 1985 r CAIRO, May 1985, Page 39-60 PDF (3.23 MB) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/asat.1985.26465 | ||||
View on SCiNiTO | ||||
Author | ||||
A. M. EL-KERSH | ||||
Lecturer,Mechanical Engineering Dept.,Faculty of Engineering and Technology,Minia University,Minia,Egypt. | ||||
Abstract | ||||
An attempt has been made to develop a method for predicting the development of turbulent boundary layers in adverse pressure gradient. Simple calculation procedure is presented by incorp-orating a deceleration rate parameter into boundary layer equations. The compressibility effect of the flow is considered° by adopting the Mach number in the momentum and skin friction relations. The predictions of the boundary layers are in good agreement with available experimental results,which validates the calculational technique. | ||||
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