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

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 resu...

Full description

Saved in:
Bibliographic Details
Main Authors: Al-Kayiem, Hussain H., Darwish, A.A., Mahmod, Y.A.
Format: Citation Index Journal
Published: University of Technology - Baghdad 1998
Subjects:
Online Access:http://eprints.utp.edu.my/4123/1/1.pdf
http://eprints.utp.edu.my/4123/
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items