A computational model for predicting damage evolution in laminated composite plates /

The feasibility of producing a model capable of predicting the evolution of interface degradation, matrix cracking, and delimitation at multiple sites in laminated continuous fiber composite plates subjected to monotonic loading, while still being computationally tenable is shown herein. Due to the...

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Bibliographic Details

Main Author:	Phillips, Mark Lane, 1972-
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 1999.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy