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ROTORCRAFT AERODYNAMIC AND AEROACOUSTIC MODELLING USING VORTEX PARTICLE METHODS
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| 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 |
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