Aerodynamic performance of shark skin shape vortex generator
The performance of NACA 4415 airfoils with counter rotating triangular or shark skin shape sub-boundary layer vortex generators were evaluated. This is relevant to the improvement of lift-to-drag ratio of the airfoil which will contribute to development of a more efficient airfoil. The lift and drag...
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| Main Authors: | , , , , |
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| Format: | Book Section |
| Language: | English |
| Published: |
Springer
2020
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| Online Access: | http://psasir.upm.edu.my/id/eprint/87780/1/ABSTRACT.pdf http://psasir.upm.edu.my/id/eprint/87780/ https://link.springer.com/chapter/10.1007/978-981-15-4756-0_10 |
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