http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Multilayer theory for delamination analysis of a composite curved bar subjected to end forces and end moments
National Aeronautics and Space Administration.
Scientific and Technical Information Division.
"Performing organization report number: H-1490"--Technical rept. documentation p.
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.
Includes bibliographical references (page 14).