ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE METHODS

Opoku, D; Triantos, D; Nitzsche, F; Voutsinas, S

dc.contributor.author	Opoku, D	en
dc.contributor.author	Triantos, D	en
dc.contributor.author	Nitzsche, F	en
dc.contributor.author	Voutsinas, S	en
dc.date.accessioned	2014-03-01T01:51:43Z
dc.date.available	2014-03-01T01:51:43Z
dc.date.issued	2002	en
dc.identifier.uri	https://dspace.lib.ntua.gr/xmlui/handle/123456789/26408
dc.relation.uri	http://rotorcraft.mae.carleton.ca/php/people/fn_papers/Proc_ICAS02.pdf	en
dc.subject	Computational Efficiency	en
dc.subject	Particle Method	en
dc.title	ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE METHODS	en
heal.type	journalArticle	en
heal.publicationDate	2002	en
heal.abstract	The initial development of a combined active aeroelastic aeroacoustic rotorcraft code is discussed. The GENeral Unsteady Vortex Particle code (GENUVP) is used as the aerodynamic component of the combined code. A brief discussion of the theory behind GENUVP's use of an unsteady panel method with a vortex particle wake is presented. Modifications to GENUVP to increase its computational efficiency are	en