Effects of internal Acoustic Excitation on the Improvementof Airfoil Performance
The effect of internal acoustic excitation on the leading-edge, separated boundary layers and the aerodynamic performance of NACA23015 cross section airfoil are examined as a function of excitation location with ranging frequency range (50-400) Hz of the introduced acoustic. Tests are separately con...
Saved in:
| Main Author: | |
|---|---|
| Format: | article |
| Language: | EN |
| Published: |
Al-Khwarizmi College of Engineering – University of Baghdad
2007
|
| Subjects: | |
| Online Access: | https://doaj.org/article/d8b0587a497d427f9b3a7b7c8f5dae66 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|