Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments
By: William L. Ko and Raymond H. Jackson.
Contributors: Jackson, Raymond H.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4139.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, DC]; [Springfield, VA
Language: eng
Format: Microform
Number of pages: 25
Subjects: Composite materials -- Delamination.; Bars.; Bending.; Composite materials.; Delaminating.; Loads (Forces); Performance prediction.; Stress analysis.
Notes: Shipping list no.: 90-0577-M.

"Performing organization report no.: H-1490"--Technical rept. documentation p.

Includes bibliographical references (p. 14).

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.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

RTOP-532-09-01.