Aerodynamic Investigation of NACA 0020 Airfoil with Extended and Serrated Trailing Edge at Various Turbulent Intensities

dc.contributor.guide	Nadaraja Pillai, S
dc.coverage.spatial	Engi
dc.creator.researcher	Livya, E
dc.date.accessioned	2024-11-08T07:50:49Z
dc.date.available	2024-11-08T07:50:49Z
dc.date.awarded	2024
dc.date.completed	2023
dc.date.registered	2019
dc.description.abstract	Abstract Included
dc.description.note	References p.187, Appendix p.188-189
dc.format.accompanyingmaterial	DVD
dc.format.dimensions	30 cm
dc.format.extent	xix, 189p
dc.identifier.uri	http://hdl.handle.net/10603/600099
dc.language	English
dc.publisher.institution	School of Mechanical Engineering
dc.publisher.place	Thanjavur
dc.publisher.university	SASTRA University
dc.relation	Engineering Aerospace
dc.rights	university
dc.source.university	University
dc.subject.keyword	Airfoil Trailing Edge Modification
dc.subject.keyword	Engineering
dc.subject.keyword	Engineering Aerospace
dc.subject.keyword	Engineering and Technology
dc.subject.keyword	Wind Tunnel Testing
dc.title	Aerodynamic Investigation of NACA 0020 Airfoil with Extended and Serrated Trailing Edge at Various Turbulent Intensities
dc.title.alternative
dc.type.degree	Ph.D.