Bolt Bearing Behavior of Highly Loaded Polymer Matrix Composite Joints at Elevated Temperatures with and Without Clamp-Up

Journal of Composites Technology and Research

Volumn 22, Issue 1, 2000, Pages 33-39

  Wright, Richard J ^a   Johnson, W Steven ^b   Sacks, Serena ^b   Ahmad, Hafiz ^c  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

^b Georgia Institute of Technology   (United States)

^c Lockheed Martin Aeronautical Systems   (Georgia)

Author keywords

Aging; Bolt bearing; Bypass; Creep; Joints

Indexed keywords

EID: 0002494769     PISSN: 08846804     EISSN: None     Source Type: Journal    
DOI: 10.1520/ctr10622j     Document Type: Article

References (4)

1. Crews, J. H., Jr. and Naik, R. V. A., "Failure Analysis of a Graphite/Epoxy Laminate Subjected to Bolt Bearing Loads," Composite Materials: Fatigue and Failure, ASTM STP 907, H. T. Hahn, Ed , American Society for Testing and Materials, West Conshohocken, PA, 1986, pp. 115-133.
2. MIL-HDBK-5G, Military Handbook: Metallic Materials and Elements for Aerospace Vehicle Structures, 1994.
3. Sacks, S. and Johnson, W. S., "Effects of Thermal Aging on the Mechanical Behavior of K3B Matrix Material," Proceedings of the 11th American Society for Composites Technical Conference, W. S. Johnson, Ed., Technomic Publishing, Lancaster, PA, 1996, pp. 666-674.
4. "Standard Test Method for Plane-Strain Fracture Toughness of Metallic Materials," Annual Book of ASTM Standards, Vol. 03.01, 1995, pp. 412-426.