Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load
By: S.A. Salpekar, I.S. Raju, and T.K. O'Brien.
Contributors: Raju, I. S.; O'Brien, T. Kevin.; Langley Research Center.; United States. Army Aviation Research and Technology Activity.
Series: NASA technical memorandum -- 102592.; AVSCOM technical memorandum -- 90-B-003.; AVSCOM technical memorandum -- 90-B-3.
Publisher: National Aeronautics and Space Administration, Langley Research Center; US Army Aviation Systems Command, Aviation R&T Activity; National Technical Information Service, distributor
Published: 1990
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 49
Subjects: Laminated materials -- Stress corrosion.; Composite materials -- Delamination.; Delaminating.; Epoxy matrix composites.; Finite element method.; Glass fiber reinforced plastics.; Laminates.; Loads (Forces); Strain energy release rate.; Stress analysis.
Notes: Cover title.

Distributed to depository libraries in microfiche.

"March 1990."

Includes bibliographical references (p. 17-18).

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

National Aeronautics and Space Administration; U.S. Army Aviation Systems Command. 505-63-01-05.