http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory
National Aeronautics and Space Administration,
1 online resource (408 pages) : color illustrations.
Title from title screen (viewed Feb. 27, 2015).
Includes bibliographical references (pages 131-138).
Technical memorandum April 2013-April 2014.
Sponsored by the National Aeronautics and Space Administration 869021.04.07.01.13