Postbuckling delamination of a stiffened composite panel using finite element methods /

Bibliographic Details

Main Authors:	Natsiavas, S. (Author), Babcock, Charles D. (Author), Knauss, Wolfgang Gustav (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Pasadena, California : California Institute of Technology, August, 1987.
Series:	NASA contractor report ; NASA CR-182803.
Subjects:	Buckling. Delaminating. Finite element method. Compression loads. Plate theory.
Online Access:	https://purl.fdlp.gov/GPO/gpo57134