Constitutive modeling of the facesheet to core interface in honeycomb sandwich panels subject to mode I delamination /

Bibliographic Details

Main Author:	Höwer, Daniel (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, August 2017.
Series:	NASA technical memorandum ; 2017-219470.
Subjects:	Carbon fibers. Delaminating. Finite element method. Honeycomb structures. Sandwich structures.
Online Access:	https://purl.fdlp.gov/GPO/gpo85740