GARTEUR (AD) AG-26: Navier-Stokes computations of 3D transonic flow for a wing/fuselage configuration

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dc.contributor.authorBrandsma, F.J.en_US
dc.date.accessioned2013-10-23T08:18:38Z
dc.date.available2013-10-23T08:18:38Z
dc.date.issued2003en_US
dc.identifier.otherNLR-TP-2003-191en_US
dc.identifier.urihttp://hdl.handle.net/10921/616
dc.language.isonlen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2003-191en_US
dc.subject.otherComputational fluid dynamicsen_US
dc.subject.otherAeronauticsen_US
dc.titleGARTEUR (AD) AG-26: Navier-Stokes computations of 3D transonic flow for a wing/fuselage configurationen_US

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