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Computational Procedure to Investigate the Boundary Layer Growth Parameters on Conventional Aerfoil

Al-Kayiem, Hussain H. and Darwish, A.A. and Mahmod, Y.A. (1998) Computational Procedure to Investigate the Boundary Layer Growth Parameters on Conventional Aerfoil. [Citation Index Journal]

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Abstract

This work includes computational procedure to solve Navier-Stocks equation of viscous flow over 4415 airfoil. Three computer programs have been established to predict the boundary layer growth parameters over the selected airfoil at different angles of attack and different Reynolds numbers. The results have demonstrated that the procedure is capable to predict the boundary layer parameters and position of the separation point is determined correctly at each tested angle of attack.

Item Type:Citation Index Journal
Subjects:T Technology > TJ Mechanical engineering and machinery
U Military Science > U Military Science (General)
Academic Subject One:Academic Department - Mechanical Engineering - fluid flow
Departments / MOR / COE:Departments > Mechanical Engineering
ID Code:4123
Deposited By: Assoc Prof Hussain H. Al-Kayiem
Deposited On:28 Feb 2013 14:34
Last Modified:28 Feb 2013 14:34

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