Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm

Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm

Film cooling is vital to gas turbine blades to protect them from high temperatures and hence high thermal stresses. In the current work, optimization of film cooling parameters on a flat plate is investigated numerically. The effect of film cooling parameters such as inlet velocity direction, latera...

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Bibliographic Details
Main Authors: Ahmed M. Elsayed, Farouk M. Owis, M. Madbouli Abdel Rahman
Format: Article
Language:English
Published: Wiley 2013-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2013/859465
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