Computational aero-acoustic analysis of blade-vortex interaction (BVI) in helicopter

dc.contributor.advisor	Narayanan, Vinod
dc.contributor.author	Syriac, John Sherjy
dc.date.accessioned	2019-08-29T09:48:15Z
dc.date.available	2019-08-29T09:48:15Z
dc.date.issued	2019
dc.identifier.citation	Syriac, John Sherjy (2019). Computational aero-acoustic analysis of blade-vortex interaction (BVI) in helicopter. Gandhinagar: Indian Institute of Technology Gandhinagar, 53p. (Acc. No.: T00431).
dc.identifier.uri	https://repository.iitgn.ac.in/handle/123456789/4775
dc.description.statementofresponsibility	by John Sherjy Syriac
dc.format.extent	xv, 53p.: ill.; 30 cm.
dc.language.iso	en_US
dc.publisher	Indian Institute of Technology Gandhinagar
dc.subject	17210041
dc.subject	Mechanical Engineering
dc.subject	NACA 23012 Airfoil
dc.subject	Near Trailing Edge Air Suction
dc.subject	Vortex Diffusion
dc.subject	Hover Configuration
dc.subject	Computational Fluid Dynamics
dc.title	Computational aero-acoustic analysis of blade-vortex interaction (BVI) in helicopter
dc.type	Thesis
dc.contributor.department	Mechanical Engineering
dc.description.degree	M.Tech.