Research Catalog

Title

An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / Michael P. Nemeth.

Author

Nemeth, Michael P.

Publication

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.

Details

Additional Authors

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

Description

1 online resource (60 pages) : color illustrations.

Series Statement

NASA/TM ; 2013-217999

Uniform Title

NASA technical memorandum ; 217999.

Subject

• Anisotropy
• Axial compression loads
• Cylindrical shells
• Inhomogeneity
• Laminates
• Sandwich structures

Note

• Title from title screen (viewed on Feb. 12, 2014).
• "May 2013."

Bibliography (note)

• Includes bibliographical references (page 19).

Funding (note)

• Sponsored by the National Aeronautics and Space Administration

Call Number

GPO Internet NAS 1.15:2013-217999

OCLC

marcive870332862

Author

Nemeth, Michael P., author.

Title

An Approximate solution and master curves for buckling of symmetrically laminated composite cylinders / Michael P. Nemeth.

Publisher

Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.

Type of Content

text

Type of Medium

computer

Type of Carrier

online resource

Series

NASA/TM ; 2013-217999

NASA technical memorandum ; 217999.

Bibliography

Includes bibliographical references (page 19).

Funding

Sponsored by the National Aeronautics and Space Administration 869021.04.07.01.13

; L-20250

Connect to:

https://purl.fdlp.gov/GPO/gpo45682

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 1.15:2013-217999