Aerodynamic performance of shark skin shape vortex generator

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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Dades bibliogràfiques
Autors principals:	Zulkefli, Nur Faraihan, Ahamat, Mohamad Asmidzam, Mohd Safri, Nurul Fatihah, Mohd Nur, Nurhayati, Mohd Rafie, Azmin Shakrine
Format:	Book Section
Idioma:	English
Publicat:	Springer 2020
Accés en línia:	http://psasir.upm.edu.my/id/eprint/87780/1/ABSTRACT.pdf

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