Static and fatigue strengths of a G40-800/5260 carbon fiber/bismaleimide composite material at room temperature and 150°C

Journal of Composite Materials

Volumn 42, Issue 7, 2008, Pages 655-679

  Shimokawa, Toshiyuki ^a   Kakuta, Yoshiaki ^a   Hamaguchi, Yasumasa ^a   Aiyama, Takenori ^b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b TOYOTA MOTOR CORPORATION   (Japan)

Author keywords

Bismaleimide; CFRP; Fatigue strength; Fiber dominant; G40 800 5260; High temperature; Matrix dominant; Non hole specimen; Notched strength criterion; Open hole specimen; Practicality; Room temperature; Static strength

Indexed keywords

CARBON FIBERS; COMPRESSIVE STRENGTH; FATIGUE OF MATERIALS; TENSILE TESTING;

BISMALEIMIDE COMPOSITE; FATIGUE STRENGTHS; MATRIX-DOMINANT PROPERTIES; ROOM TEMPERATURE;

COMPOSITE MATERIALS;

EID: 41149113348     PISSN: 00219983     EISSN: 1530793X     Source Type: Journal    
DOI: 10.1177/0021998308088605     Document Type: Article

References (27)

1. F-22 Raptor Materials and Process. (2005). http://www.globalsecurity.org/ military/systems/ aircraft/f-22-mp.htm. 19-12-2005.
2. High-Speed Research, F22 Air Dominance for the 21st Century. (2004). http://www. allstar.fiu.edu/aero/f22raptor.html. ALLSTAR, 21-3-2004.
3. Shimokawa, T., Hamaguchi, Y., Kakuta, Y. and Katoh, H. (1999). Effect of Isothermal Aging on Ultimate Strength of High Temperature Composite Materials for SST Structures, Journal of Composite Materials, 33 (12). 1104-1118.
4. Shimokawa, T., Katoh, H., Hamaguchi, Y., Sanbongi, S., Mizuno, H., Nakamura, H., Asagumo, R. and Tamura, H. (2002). Effect of Thermal Cycling on Microcracking and Strength Degradation of High-Temperature Polymer Composite Materials for Use in Next-Generation SST Structures, Journal of Composite Materials, 36 (7). 885-895.
5. Marais, C., Shimokawa, T. and Katoh, H. (2001). ID-1024 Compressive Strength/ Degradation Relationship of Carbon/BMI Composites After Thermal Cycling and Aging for the Second Generation SST Structures, Proc. 13th International Conference on Composite Materials (CD-ROM), Beijing.
6. Katoh, H., Shimokawa, T., Tsuda, H., Sakai, A. and Asagumo, R. (2000). Bearing Creep Behavior of a Carbon/Bismaleimide Composite Material for the Next-Generation Supersonic Transport, Proc. 9th United States - Japan Conf. on Composite Materials, Mishima, Japan Society for Composite Materials and American Society for Composites, pp. 603-610.
7. Xian, X.J. and Choy, C.L. (1994). Fatigue Fracture Behavior of Carbon-Fiber-Reinforced Modified Bismaleimide Composites, Composite Science and Technology, 52: 93-98.
8. Gathercole, N., Reiter, H., Adam, T. and Harris, B. (1994). Life Prediction for Fatigue of T800/5245 Carbon-Fiber Composites I. Constant-Amplitude Loading, International Journal of Fatigue, 16: 523-532.
9. Adam, T., Gathercole, N., Reiter, H. and Harris, B. (1994). Life Prediction for Fatigue of T800/5245 Carbon-Fiber Composites: II. Variable-Amplitude Loading, International Journal of Fatigue, 16: 533-547.
10. Hirano, K. (2001). ID-1299 Long-Term Durability Performance for Advanced High Temperature Polymer Matrix Composites, Proc. 13th International Conference on Composite Materials (CD-ROM), Beijing.
11. Kobayashi, S., Ogihara, S., Terada, K., Takeda, N. and Kobayashi, A. (2001). Microscopic Damage Progress in Carbon/Bismaleimide Cross-Ply Laminate Under Fatigue Loading, Proc. 21st International Committee on Aeronautical Fatigue Symposium, Toulouse, pp. 929-940.
12. Coats, T.W. and Harris, C.E. (1995). Experimental Verification of a Progressive Damage Model for IM7/5260 Laminates Subjected to Tension-Tension Fatigue, Journal of Composite Materials, 29 (3). 280-305.
13. Tyahla, S.T. and McClellan Jr, P.S. (1988). Durability and Damage Tolerance of Bismaleimide Composites - Volume I: Technical Report. AFWAL-TR-88-3026, Wright-Patterson Air Force Base.
14. Johnston, W.M. and Gates, T.S. (1998). The Effects of Stress and Temperature on the Open-Hole Tension Fatigue Behavior of a Graphite/Bismaleimide Composite, Composite Materials: Fatigue and Fracture, ASTM STP 1330, American Society for Testing and Materials, pp. 179-198.
15. Shimokawa, T., Hamaguchi, Y. and Katoh, H. (1999). Effect of Moisture Absorption on Hot/Wet Compressive Strength of T800H/PMR-15 Carbon Polyimide, Journal of Composite Materials, 33 (18). 1685-1698.
16. Shimokawa, T., Kakuta, Y., Saeki, D. and Kogo, Y. (2007). Carbon Plain-Weave Fabric Low-Temperature Vacuum Cure Epoxy Composite: Static and Fatigue Strength at Room and High Temperatures and Practicality Evaluation, Journal of Composite Materials, 41 (18). 2245-2265.
17. Niu, M.C.Y. (1996). Composite Airframe Structures - Practical Information and Data -, Hong Kong Conmilit Press Ltd., p. 75.
18. Pilato, L.A. and Michno, M.J. (1994). Advanced Composite Materials, Springer-Verlag, p. 129 and p. 151.
19. Rosenfeld, M.S. and Gause, L.W. (1981). Compression Fatigue Behavior of Graphite/Epoxy in the Presence of Stress Raisers, Fatigue of Fibrous Composite Materials, ASTM STP 723, American Society for Testing and Materials, pp. 174-196.
20. Nagao, Y., Iwahori, Y., Hirano, Y. and Aoki, Y. (2007). Low Cost Composite Wing Structure Manufacturing Technology Development Program in JAXA, Proc. 16th International Conference on Composite Materials (CD-ROM), Kyoto.
21. Japan Aerospace Exploration Agency. (2007). Advanced Composites Database System: JAXA-ACDB, Ver. 06-1, http://www.jaxa-acdb.com/.
22. Kakuta, Y., Sanbongi, S., Shimokawa, T., Hamaguchi, Y., Yamamoto, M. and Mitsuma, H. (1994). Evaluation of Static Strength of T800H/PMR-15 Carbon/Polyimide Laminates at Room Temperature and 300°C, Technical Report of National Aerospace Laboratory TR-1254, National Aerospace Laboratory (in Japanese).
23. Whitney, J.M. and Nuismer, R.J. (1974). Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations, Journal of Composite Materials, 8: 253-265.
24. Pipes, R.B., Wetherhold, R.C. and Gillespie Jr, J.W. (1979). Notched Strength of Composite Materials, Journal of Composite Materials, 13: 148-160.
25. Tan, S.C. (1988). Effective Stress Fracture Models for Unnotched and Notched Multidirectional Laminates, Journal of Composite Materials, 22: 322-340.
26. Eriksson, I. and Aronsson, C.G. (1990). Strength of Tensile Loaded Graphite/Epoxy Laminates Containing Cracks, Open and Filled Holes, Journal of Composite Materials, 24: 456-482.
27. Gillespie Jr, J.W. and Carlsson, L.A. (1988). Influence of Finite Width on Notched Laminate Strength Predictions, Composite Science and Technology, 32: 15-30.