Effect of Using Bumps on Wings Aerodynamic Characteristics at Low Reynolds Numbers
The effect of using bumps on the aerodynamic characteristics of airfoil at low Reynolds numbers is presented in this research. A theoretical study was done on the (NACA 4418) airfoil consist of bumps that have radius (2% c) on the upperand lower surfaces at (Re=25×103). Experimental study was also d...
| Format: | Article |
|---|---|
| Language: | English |
| Published: |
Unviversity of Technology- Iraq
2010-06-01
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| Series: | Engineering and Technology Journal |
| Online Access: | https://etj.uotechnology.edu.iq/article_27781_14e7defafe902a0a47067518523c5583.pdf |