Fatigue debonding characterization in composite skin/stringer configurations
By: Michael K. Cvitkovich, T. Kevin O'Brien, Pierre J. Minguet.
Contributors: O'Brien, T. Kevin.; Minguet, Pierre J.; Langley Research Center.
Series: NASA technical memorandum -- 110331.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Fatigue tests.; Debonding (Materials); Composite structures.; Flanges.; Skin (Structural member); Bonded joints.; Crack initiation.; Delaminating.; Graphite-epoxy composites.; Resin matrix composites.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 98-0007-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.