Damage growth in stitched graphite/epoxy laminates under mode I fracture and compression loading

American Society of Mechanical Engineers, Aerospace Division (Publication) AD

Volumn 52, Issue , 1996, Pages 39-43

  Sharma, Suresh K ^a   Sankar, Bhavani V ^b  

^a GENERAL ELECTRIC COMPANY   (United States)

^b UNIVERSITY OF FLORIDA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPRESSION TESTING; DEFORMATION; FRACTURE MECHANICS; GRAPHITE; IMPACT TESTING; REINFORCEMENT;

DAMAGE GROWTH; FRACTURE AND COMPRESSION LOAD; GRAPHITE/EPOXY LAMINATES;

LAMINATED COMPOSITES;

EID: 3643085557     PISSN: 07334230     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (5)

1. Mechanical Engineering, Vol. 117/No 10, Oct 1995, News and Notes, page 14
2. Sharma, S.K. and Sankar, B.V., 1995 "Fracture Toughness of Stitched Graphite/Epoxy Uniweave Laminates," Proceedings of the symposium 'Durability and Damage Tolerance of Composite' held during ASME winter annual meeting, ASME International Mechanical Engineering Congress and Exposition in San Francisco, November 1995.
3. Sharma, S.K. and Sankar, S.V., 1995, "Effects of Through-the-Thickness Stitching on Impact and Interlaminar Fracture Properties of Textile Graphite/Epoxy Laminates," NASA Contractor Report 195042.
4. Kwon, Y.S. and Sankar, B.V., 1992, "Indentation-flexure and low-velocity impact damage in graphite epoxy laminates," NASA Contractor Report 187624.
5. Madan, R.C., 1988, "Composite Transport Wing Technology Development," NASA Contractor Report 178409.