Cover Image

Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments /

Bibliographic Details
Main Author: Ko, William L.
Corporate Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors: Jackson, Raymond H.
Format: Government Document Microform Book
Language:English
Published: [Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1989.
Series:NASA technical memorandum ; 4139.
Subjects:
Composite materials > Delamination.
Bars.
Bending.
Composite materials.
Delaminating.
Loads (Forces)
Performance prediction.
Stress analysis.
Online Access:https://purl.fdlp.gov/GPO/LPS70454
Description
Item Description:"Performing organization report number: H-1490"--Technical rept. documentation p.
"September 1989."
Shipping list number: 90-0577-M.
Microform.
Physical Description:25 pages : illustrations ; 28 cm.
Also available via Internet from the NASA Technical Report Server web site. Address as of 6/6/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900003353%5F1990003353.pdf; current access available via PURL.
Bibliography:Includes bibliographical references (page 14).