Influence of specimen preparation and specimen size on composite transverse tensile strength and scatter
By: T. Kevin O'Brien ... [et al.].
Contributors: O'Brien, T. Kevin.; Langley Research Center.
Series: NASA/TM -- 2001-211030.; ARL-TR -- 2540.; NASA technical memorandum -- 211030.; ARL-TR (Aberdeen Proving Ground, Md.) -- 2540.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information (CASI)
Published: 2001
Place of publication: Hampton, Va; Hanover MD
Language: eng
Format: Microform
Subjects: Epoxy matrix composites.; Tensile strength.; Cracking (Fracturing); Glass.; Bend tests.
Notes: Shipping list no.: 2003-0056-M.

Also available via Internet from the NASA web site. Address as of 2/28/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm211030.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.