Aerodynamic performance of shark skin shape vortex generator

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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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Bibliographic Details
Main Authors:	Zulkefli, Nur Faraihan, Ahamat, Mohamad Asmidzam, Mohd Safri, Nurul Fatihah, Mohd Nur, Nurhayati, Mohd Rafie, Azmin Shakrine
Format:	Book Section
Language:	English
Published:	Springer 2020
Online Access:	http://psasir.upm.edu.my/id/eprint/87780/ http://psasir.upm.edu.my/id/eprint/87780/1/ABSTRACT.pdf

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