Aerodynamic efficiency enhancement for asymmetric profiles

BOSTAN, Viorel; GUŢU, Marin; ODAINÂI, Valeriu

dc.contributor.author	BOSTAN, Viorel
dc.contributor.author	GUŢU, Marin
dc.contributor.author	ODAINÂI, Valeriu
dc.date.accessioned	2021-04-07T09:02:24Z
dc.date.available	2021-04-07T09:02:24Z
dc.date.issued	2009
dc.identifier.citation	BOSTAN, Viorel, GUŢU, Marin, ODAINÂI, Valeriu. Aerodynamic efficiency enhancement for asymmetric profiles. In: 22nd International Conference on Innovative Manufacturing Engineering and Energy - IManE&E 2018. Sect. Mechanical and Manufacturing Equipment Devices and Instrumentation: proc. MATEC Web Conf., 2018, V. 178, Art. Nr 06022.	en_US
dc.identifier.uri	https://doi.org/10.1051/matecconf/201817806022
dc.identifier.uri	http://repository.utm.md/handle/5014/14033
dc.description	Access full text: https://doi.org/10.1051/matecconf/201817806022	en_US
dc.description.abstract	This paper presents a solution for enhancement of aerodynamic efficiency for asymmetric airfoils. In order to increase the lift and reduce the drag forces for a blade segment, a groove was created on its surface. There were carried out experiments consisting in the analysis of two asymmetric airfoil segments of the same type in the wind tunnel. One segment was designed with the groove and the other without it. The optimum location of the groove was determined by means of CFD analysis. Simulation results were compared to test results and the CFD analysis model was validated.	en_US
dc.language.iso	en	en_US
dc.publisher	EDP Sciences	en_US
dc.rights	Attribution-NonCommercial-NoDerivs 3.0 United States	*
dc.rights.uri	http://creativecommons.org/licenses/by-nc-nd/3.0/us/	*
dc.subject	aerodynamic efficiency	en_US
dc.subject	airfoils	en_US
dc.subject	blades	en_US
dc.title	Aerodynamic efficiency enhancement for asymmetric profiles	en_US
dc.type	Article	en_US