Buckling analysis for stiffened anisotropic circular cylinders based on Sanders' nonlinear shell theory / Michael P. Nemeth.

Author/creator Nemeth, Michael P. author.
Other author Langley Research Center, issuing body.
Other author United States. National Aeronautics and Space Administration sponsoring body.
Format Electronic
PublicationHampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.
Description1 online resource (408 pages) : color illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo55308

SeriesNASA/TM ; 2014-218176
NASA technical memorandum 2014-218176. ^A467613
General noteTitle from title screen (viewed Feb. 27, 2015).
General note"March 2014."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (pages 131-138).
Report noteTechnical memorandum April 2013-April 2014.
Funding informationSponsored by the National Aeronautics and Space Administration 869021.04.07.01.13
Funding informationL-20320 [NF1676L-17349]
GPO item number0830-D (online)
Govt. docs number NAS 1.15:2014-218176

Availability

Library Location Call Number Status Item Actions
Electronic Resources Access Content Online ✔ Available