A study of grid convergence issues for the simulation of the massively separated flow around a stalled airfoil using DES and related methods

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dc.contributor.authorWeinman, K.A.en_US
dc.contributor.authorVen, H. van deren_US
dc.contributor.authorMockett, C.R.en_US
dc.contributor.authorKnopp, T.A.en_US
dc.contributor.authorKok, J.C.en_US
dc.contributor.authorPerrin, R.T.E.en_US
dc.contributor.authorThiele, F.H.en_US
dc.date.accessioned2012-03-14T09:52:57Z
dc.date.available2012-03-14T09:52:57Z
dc.date.issued2006en_US
dc.identifier.otherNLR-TP-2006-436en_US
dc.identifier.urihttp://hdl.handle.net/10921/353
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2006-436en_US
dc.subject.otherComputational fluid dynamicsen_US
dc.subject.otherNumerical analysisen_US
dc.titleA study of grid convergence issues for the simulation of the massively separated flow around a stalled airfoil using DES and related methodsen_US

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