Fatigue life methodology for bonded composite skin/stringer configurations
By: Ronald Krueger ... [et al.].
Contributors: Krueger, Ronald.; Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2001-210842.; ARL-TR -- 2432.; NASA technical memorandum -- 210842.; ARL-TR (Aberdeen Proving Ground, Md.) -- 2432.
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: Fatigue life.; Composite structures.; Debonding (Materials); Flanges.; Fatigue tests.; Finite element method.
Notes: Shipping list no.: 2002-0157-M.

Also available via Internet from the NASA web site. Address as of 10/7/02: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm210842.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2001?] 1 microfiche.