Cover Image

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
Description
Item Description:Title from title screen (viewed on Feb. 12, 2014).
"May 2013."
Physical Description:1 online resource (60 pages) : color illustrations.
Bibliography:Includes bibliographical references (page 19).