Effects of internal Acoustic Excitation on the Improvement of 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 co...
Enregistré dans:
| Auteur principal: | |
|---|---|
| Format: | article |
| Langue: | EN |
| Publié: |
Al-Khwarizmi College of Engineering – University of Baghdad
2007
|
| Sujets: | |
| Accès en ligne: | https://doaj.org/article/8ea9d0231a7749d9b62ba1d04aac19ab |
| Tags: |
Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!
|