http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
Approximate solution and master curves for buckling of symmetrically laminated composite cylinders
National Aeronautics and Space Administration,
1 online resource (60 pages) : color illustrations.
Title from title screen (viewed on Feb. 12, 2014).
Includes bibliographical references (page 19).
Sponsored by the National Aeronautics and Space Administration 869021.04.07.01.13