Innovative design of composite structures
Subtitle: the use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes
By: M.W. Hyer, H.H. Lee.
Contributors: Lee, H. H.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA/CR-186454.
Publisher: College of Engineering, Virginia Polytechnic Institute and State University; National Aeronautics and Space Administration
Published: 1990
Place of publication: Blacksburg, VA; [Washington, D.C
Language: eng
Format: Microform
Subjects: Buckling.; Composite structures.; Fiber orientation.; Holes (Mechanics); Load distribution (Forces); Perforated plates.
Notes: "Performance period: February 16, 1989-August 15, 1989."

Shipping list no.: 90-0859-M.

"March 1990."

Also available via Internet from the NASA Technical Report Server web site. Address as of 3/9/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900010819%5F1990010819.pdf; current access available via PURL.

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