A nonlinear beam finite element for curved and twisted composite helicopter blade

Simple item page
dc.contributor.authorSkladanek, Y.
dc.contributor.authorCranga, P.
dc.contributor.authorFerraris, G.
dc.contributor.authorJacquet, G.
dc.contributor.authorDufour, R.
dc.date.accessioned2016-07-01T13:10:02Z
dc.date.available2016-07-01T13:10:02Z
dc.date.issued2010
dc.identifier.otherY.SKLADANEK_065_paper
dc.identifier.urihttp://hdl.handle.net/20.500.11881/873
dc.language.isoen
dc.subject.otherDynamics
dc.titleA nonlinear beam finite element for curved and twisted composite helicopter blade

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
Y.SKLADANEK_065_paper.pdf
Size:
203.87 KB
Format:
Adobe Portable Document Format
Download

Collections

Papers