Static aeroelastic simulation of military aircraft configuration in transonic flow

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dc.contributor.authorPrananta, B.B.en_US
dc.contributor.authorTjatra, I.W.en_US
dc.contributor.authorSpekreijse, S.P.en_US
dc.contributor.authorKok, J.C.en_US
dc.contributor.authorMeijer, J.J.en_US
dc.date.accessioned2013-10-23T10:13:49Z
dc.date.available2013-10-23T10:13:49Z
dc.date.issued2001en_US
dc.identifier.otherNLR-TP-2001-346en_US
dc.identifier.urihttp://hdl.handle.net/10921/776
dc.language.isoenen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;2001-346en_US
dc.subject.otherAeroelasticity / unsteady flowen_US
dc.subject.otherMilitary operations researchen_US
dc.titleStatic aeroelastic simulation of military aircraft configuration in transonic flowen_US

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