Effects of stacking sequence on microscopic fatigue damage development in quasi-isotropic CFRP laminates with interlaminar-toughened layers

Composites Science and Technology

Volumn 59, Issue 9, 1999, Pages 1387-1398

  Ogihara, Shinji ^a   Takeda, Nobuo ^b   Kobayashi, Satoshi ^b   Kobayashi, Akira ^a  

^a TOKYO UNIVERSITY OF SCIENCE   (Japan)

^b UNIVERSITY OF TOKYO   (Japan)

Author keywords

B. Fatigue; C. Delamination; C. Transverse crack; Interlaminar toughened laminate; Quasi isotropic CFRP laminate

Indexed keywords

CRACK PROPAGATION; DELAMINATION; EPOXY RESINS; FATIGUE OF MATERIALS; LAMINATES; OPTICAL MICROSCOPY; POLYAMIDES; TENSILE PROPERTIES; X RAY RADIOGRAPHY;

INTERLAMINAR TOUGHENED LAMINATE; QUASI ISOTROPIC LAMINATE; TRANSVERSE CRACK;

CARBON FIBER REINFORCED PLASTICS;

ANALYSIS; DAMAGE; FATIGUE; FIBER REINFORCED COMPOSITE; INTERLAMINAR PROPERTY; LOADING; MICROSCOPY;

EID: 0032835244     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0266-3538(98)00180-8     Document Type: Article

References (14)

1. Talreja R. Fatigue of composite materials: damage mechanisms and fatigue-life diagrams. Proc. Roy. Soc. Lond. A378:1981;461-475.
2. Talreja R. A conceptual framework for the interpretation of fatigue damage mechanisms in composite materials. J. Comp. Tech. Res. 7:1985;25-29.
3. Masters J.E., Reifsnider K.L. An investigation of cumulative damage development in quasi-isotropic graphite/epoxy laminates. ASTM STP. 775:1980;40-62.
4. O'Brien T.K. Characterization of delamination onset and growth in a composite laminate. ASTM STP. 775:1980;140-167.
5. Wang ASD. Strength, failure and fatigue analysis of laminates. In: composites, engineering materials handbook, vol. 1. Metals Park OH: ASM International, 1987. p. 236-51.
6. Charewicz A., Daniel I.M. Damage mechanisms and accumulation in graphite/epoxy laminates. ASTM STP. 907:1986;274-297.
7. Liu S, Nairn JA. Fracture mechanics analysis of composite microcracking: experimental results in fatigue. In: Proc. 5th Tech Conf on Compos Mater. American Society for Composites, Lancaster, PA: Technomic, 1990. p. 287-95.
8. Takeda N., Ogihara S., Kobayashi A. Microscopic fatigue damage progress in CFRP cross-ply laminates. Composites. 26:1995;859-867.
9. Odagiri N, Muraki T, Tobukuro K. Toughness improved high performance Torayca prepreg T800H/3900 series. Proc 33rd International SAMPE Symposium, 1988. p. 272-83.
10. Odagiri N, Kishi H, Nakae T. T800H/3900-2 toughened epoxy prepreg system: toughening concept and mechanism. Proc American Society for Composites 6th Technical Conference, 1991. p. 43-52.
11. Takeda N., Ogihara S., Kobayashi A., Song D.-Y. Microscopic fatigue failure process in interleaved and toughness-improved CFRP cross-ply laminates. Advanced Composite Materials. 6:1997;309-326.
12. Gudmundson P., Zang W. An analytic model for thermoelastic properties of composite laminates containing transverse matrix cracks. Int. J. Solids Structure. 30:1993;3211-3231.
13. Ogihara S., Takeda N., Kobayashi S., Kobayashi A. Experimental characterization of microscopic damage initiation and growth in quasi-isotropic CFRP laminates. Trans. JSME. A62:1996;2250-2255. [in Japanese].
14. Takeda N., Niizuma H., Ogihara S., Kobayashi A. Experimental evaluation of thermal residual stress in CFRP cross-ply laminates. Materials System. 14:1995;73-78. [in Japanese].