Fatigue debonding characterization in composite skin/stringer configurations

ASTM Special Technical Publication

Volumn 1330, Issue , 1998, Pages 97-121

  Cvitkovich, Michael K ^a   O'Brien, T Kevin ^a   Minguet, Pierre J ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b BOEING COMPANY   (United States)

Author keywords

Bond strength; Composite materials; Design; Fatigue testing; Secondary bonding; Skin flange interface

Indexed keywords

EID: 11744356618     PISSN: 00660558     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1520/stp13268s     Document Type: Article

References (4)

1. Minguet, P. J., Fedro, M. J., O'Brien, T. K., Martin, R. H., Ilcewicz, L. B., Awerbuch, J., and Wang, A., "Development of a Structural Test Simulating Pressure Pillowing Effects in a Bonded Skin/ Stringer/Frame Configuration," Proceedings, Fourth NASA/DoD Advanced Composites Technology Conference, Salt Lake City, UT, June 1993.
2. Minguet, P. J. and O'Brien, T. K., "Analysis of Test Methods for Characterizing Skin/Stringer Debonding Failures in Reinforced Composite Panels," Composite Materials: Testing and Design, Twelfth Volume, ASTM STP 1274, August 1996, pp. 105-124.
3. Minguet, P. J. and O'Brien, T. K., "Analysis of Composite Skin/Stringer Failure Using a Strain Energy Release Rate Approach," Proceedings, Tenth International Conference on Composite Materials (ICCM X), Vancouver, British Columbia, Canada, August 1995, Vol. 1, pp. 245-252.
4. Peck, A. W., "Transverse Tension Fatigue Characterization of Composite Materials," presented at the Seventh ASTM Symposium on Composite Materials: Fatigue and Fracture, (ASTM STP 1330), in press.