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

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dc.contributor.authorHegen, G.H.en_US
dc.contributor.authorPuffert-Meissner, W.en_US
dc.contributor.authorDieterle, L.en_US
dc.contributor.authorVolmers, H.en_US
dc.date.accessioned2017-02-03T13:10:13Z
dc.date.available2017-02-03T13:10:13Z
dc.date.issued1999en_US
dc.identifier.otherNLR-TP-1999-104en_US
dc.identifier.urihttp://hdl.handle.net/10921/1119
dc.language.isonlen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;1999-104en_US
dc.subject.otherExperimental fluid dynamicsen_US
dc.subject.otherWindtunnelsen_US
dc.titleFlow field investigations on a wing installed Couter Rotating Ultra- high-bypass Fan engine simulator in the low speed wind tunnel DNW-LSTen_US

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