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Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory /

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, March 2014.
Series:NASA technical memorandum ; 2014-218176.
Subjects:
Nonlinear equations.
Rayleigh-Ritz method.
Shell theory.
Shell stability.
Anisotropic shells.
Donnell equations.
Online Access:https://purl.fdlp.gov/GPO/gpo55308
http://purl.fdlp.gov/GPO/gpo55308
Description
Item Description:Title from title screen (viewed Feb. 27, 2015).
"March 2014."
Physical Description:1 online resource (408 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 131-138).