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...
Saved in:
Main Authors: | , , |
---|---|
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!
|