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Fatigue and Fracture of Advanced Composite Materials
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English
Abstract
This paper presents a brief review of some of the contributing factors in design for fatigue and fracture of advanced composite materials. Consideration is given to the roles which the fiber and matrix have in the static, fatigue, and fracture response of laminated composites. The statistical aspects of failure are also discussed.
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Citation
Kaminski, B., "Fatigue and Fracture of Advanced Composite Materials," SAE Technical Paper 730337, 1973, https://doi.org/10.4271/730337.Also In
References
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- “Military Standardization Handbook, Metallic Materials and Elements for Aerospace Structures.” September 1971
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- Shockey P. D. Hofer K. E. “Development of Engineering Data for Advanced Composite Materials: Volume II-Fatigue and Load Rate Characteristics.” Technical Report AFML-TR-70-108 II Wright-Patterson AFB October 1972
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- Waddoups M. E. Jackson S. K. Rogers C. W. “The Integration of Composite Structures into Aircraft Design.” Jrl. of Composite Materials 6 April 1972
- Halpin J. C. “Introduction to Viscoelasticity.” Composite Materials Workshop Technomic Publishing Co., Inc. 1968
- Halpin J. C. Kopf J. R. Goldberg W. “Time Dependent Static Strength and Reliability for Composites.” Jrl. of Composite Materials 4 1970
- Kaminski B. E. “Effects of Specimen Geometry on the Strength of Composite Materials.” ASTM Symposium on Analysis of Test Methods for High Modulus Fibers and Composites San Antonio April 1972
- Waddoups M. E. Eisenmann J. R. Kaminski B. E. “Macroscopic Fracture Mechanics of Advanced Composite Materials.” Jrl. of Composite Materials 5 October 1971
- Eisenmann J. R. Kaminski B. E. “Fracture Control for Composite Structures.” Jrl. of Engineering Fracture Mechanics 4 1972 907 913