Research Catalog

Title

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

Author

Nemeth, Michael P.

Publication

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.

Details

Additional Authors

• Langley Research Center, issuing body.
• United States. National Aeronautics and Space Administration, sponsoring body.

Description

1 online resource (408 pages) : color illustrations.

Series Statement

NASA/TM ; 2014-218176

Uniform Title

NASA technical memorandum ; 2014-218176.

Subjects

• Donnell equations
• Anisotropic shells
• Shell stability
• Shell theory
• Rayleigh-Ritz method
• Nonlinear equations

Note

• Title from title screen (viewed Feb. 27, 2015).
• "March 2014."

Bibliography (note)

• Includes bibliographical references (pages 131-138).

Type of Report (note)

• Technical memorandum

Funding (note)

• Sponsored by the National Aeronautics and Space Administration

Call Number

GPO Internet NAS 1.15:2014-218176

OCLC

marcive904125145

Author

Nemeth, Michael P., author.

Title

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

Publisher

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2014-218176

NASA technical memorandum ; 2014-218176.

Bibliography

Includes bibliographical references (pages 131-138).

Type Of Report

Technical memorandum April 2013-April 2014.

Funding

Sponsored by the National Aeronautics and Space Administration 869021.04.07.01.13

L-20320 [NF1676L-17349]

Connect to:

https://purl.fdlp.gov/GPO/gpo55308

Added Author

Langley Research Center, issuing body.

United States. National Aeronautics and Space Administration, sponsoring body.

Gpo Item No.

0830-D (online)

Sudoc No.

NAS 1.15:2014-218176