Modelling of as manufactured geometry for prediction of impact and compression after impact behaviour of variable angle tow laminates (2014)
Attributed to:
Equipment for Multiple Projects: Testing and Visualization for Aerospace Research
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1177/0021998314534707
Publication URI: http://dx.doi.org/10.1177/0021998314534707
Type: Journal Article/Review
Parent Publication: Journal of Composite Materials
Issue: 12