Floating node method and virtual crack closure technique for modeling matrix cracking-delamination interaction /

Bibliographic Details

Main Author:	De Carvalho, N. V. (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, July 2013.
Series:	NASA contractor report ; NASA CR-218022.
Subjects:	Crack closure. Fracture mechanics. Delaminating. Ply orientation. Laminates.
Online Access:	https://purl.fdlp.gov/GPO/gpo53799 http://purl.fdlp.gov/GPO/gpo53799