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Aerodynamic interference in full helicopter configurations and assessment of noise emission: Pre-test modelling activities for the Helinovi experimental campaign

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dc.contributor.author Voutsinas, SG en
dc.contributor.author Visingardi, A en
dc.contributor.author Yin, J en
dc.contributor.author Arnaud, G en
dc.contributor.author Falchero, D en
dc.contributor.author Dummel, A en
dc.contributor.author Pidd, M en
dc.contributor.author Prospathopoulos, J en
dc.date.accessioned 2014-03-01T02:49:59Z
dc.date.available 2014-03-01T02:49:59Z
dc.date.issued 2005 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/34850
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-33746654211&partnerID=40&md5=7c68cdd83b9cc340d9e7df4731f0f6c0 en
dc.subject.other Aircraft models en
dc.subject.other Computer simulation en
dc.subject.other Flight dynamics en
dc.subject.other Noise abatement en
dc.subject.other Noise pollution en
dc.subject.other Numerical analysis en
dc.subject.other Wind tunnels en
dc.subject.other Aerodynamic interference en
dc.subject.other BO105 scaled model en
dc.subject.other Helinovi experimental en
dc.subject.other Noise emission en
dc.subject.other Helicopters en
dc.title Aerodynamic interference in full helicopter configurations and assessment of noise emission: Pre-test modelling activities for the Helinovi experimental campaign en
heal.type conferenceItem en
heal.publicationDate 2005 en
heal.abstract The aerodynamic interference aspects of full helicopter configurations are considered with regard to assessing the potential for noise reduction. The investigation is based on pretest results from numerical tools of varying complexity and code-to-code comparisons over a range of different flight conditions chosen to match anticipated wind tunnel tests in the DNW on the BO105 scaled model. This work aims at evaluating the different codes as well as at defining the appropriate context for code-to-test comparison. The main bulk of results concern this pre-test activity while some selective comparisons of post-test simulations with measurements support the discussion and conclusions of this exercise. en
heal.journalName 31st European Rotorcraft Forum en
dc.identifier.volume 2005 en
dc.identifier.spage 68.1 en
dc.identifier.epage 68.16 en


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