A modelling framework for the calculation of structural loads for fatigue life prediction in helicopter airframe components

Simple item page
dc.contributor.authorBakker, R.J.J.
dc.contributor.authorBos, M.J.
dc.contributor.authorMünninghoff, N.
dc.contributor.authorTongeren, J.H. van
dc.contributor.authorVen, H. van der
dc.date.accessioned2016-06-29T14:39:21Z
dc.date.available2016-06-29T14:39:21Z
dc.date.issued2009
dc.identifier.otherERF;2009-101154
dc.identifier.urihttp://hdl.handle.net/20.500.11881/122
dc.language.isoen
dc.publisherNational Aerospace Laboratory NLR
dc.subject.otherDynamics
dc.titleA modelling framework for the calculation of structural loads for fatigue life prediction in helicopter airframe components

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
101154.pdf
Size:
730.3 KB
Format:
Adobe Portable Document Format
Download

Collections

Papers