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...
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| Format: | Article |
| Language: | English |
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Al-Khwarizmi College of Engineering – University of Baghdad
2007-09-01
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| Series: | Al-Khawarizmi Engineering Journal |
| Online Access: | http://alkej.uobaghdad.edu.iq/index.php/alkej/article/view/633 |