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