Flow field investigations on a wing installed Couter Rotating Ultra- high-bypass Fan engine simulator in the low speed wind tunnel DNW-LST

dc.contributor.author Hegen, G.H. en_US
dc.contributor.author Puffert-Meissner, W. en_US
dc.contributor.author Dieterle, L. en_US
dc.contributor.author Volmers, H. en_US
dc.date.accessioned 2017-02-03T13:10:13Z
dc.date.available 2017-02-03T13:10:13Z
dc.date.issued 1999 en_US
dc.identifier.other NLR-TP-1999-104 en_US
dc.identifier.uri http://hdl.handle.net/10921/1119
dc.language.iso nl en_US
dc.publisher National Aerospace Laboratory NLR en_US
dc.relation.ispartofseries NLR Technical Publication;1999-104 en_US
dc.subject.other Experimental fluid dynamics en_US
dc.subject.other Windtunnels en_US
dc.title Flow field investigations on a wing installed Couter Rotating Ultra- high-bypass Fan engine simulator in the low speed wind tunnel DNW-LST en_US
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