Delamination modeling of composites for improved crash analysis [microform] / David C. Fleming.

"Finite element crash modeling of composite structures is limited by the inability of current commercial crash codes to accurately model delamination growth. Efforts are made to implement and assess delamination modeling techniques using a current finite element crash code, MSC DYTRAN. Three me...

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Bibliographic Details
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Main Author: Fleming, David C., 1967-
Corporate Author: Langley Research Center
Format: Government Document Microfilm Book
Language:English
Published: Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, [1999]
Series:NASA contractor report ; NASA CR-209725.
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Call Number: NAS 1.26:209725
NAS 1.26:209725 Available

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number: NAS 1.26:209725
NAS 1.26:209725 Restricted Place a Hold