Determination of transonic unsteady aerodynamic loads to predict the aeroelastic stability of fighter aircraft

Simple item page
dc.contributor.authorMeijer, J.J.en_US
dc.date.accessioned2017-02-14T09:46:19Z
dc.date.available2017-02-14T09:46:19Z
dc.date.issued1997en_US
dc.identifier.otherNLR-TP-1997-304en_US
dc.identifier.urihttp://hdl.handle.net/10921/1274
dc.language.isonlen_US
dc.publisherNational Aerospace Laboratory NLRen_US
dc.relation.ispartofseriesNLR Technical Publication;1997-304en_US
dc.subject.otherAeroelasticity / unsteady flowen_US
dc.subject.otherMilitary operations researchen_US
dc.titleDetermination of transonic unsteady aerodynamic loads to predict the aeroelastic stability of fighter aircraften_US

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
TP-1997-304.pdf
Size:
439.59 KB
Format:
Adobe Portable Document Format
Download

Collections

Reports