An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders /

Bibliographic Details

Main Author:	Nemeth, Michael P. (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, 2013.
Series:	NASA technical memorandum ; 217999.
Subjects:	Anisotropy. Axial compression loads. Cylindrical shells. Inhomogeneity. Laminates. Sandwich structures.
Online Access:	https://purl.fdlp.gov/GPO/gpo45682 http://purl.fdlp.gov/GPO/gpo45682