Damage resistance of the composite laminates with interlayer thermoplastic particles

Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica

Volumn 22, Issue 2, 2005, Pages 116-120

  Gao, Feng ^a   Jiao, Guiqiong ^a   Ning, Rongchang ^a   Lu, Zhixian ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Composite laminates; Damage resistance; Quasi static indentation test; Thermoplastic particle interlayer toughening; Toughening mechanism

Indexed keywords

CARBON FIBERS; COMPRESSIVE STRENGTH; CRACK PROPAGATION; DELAMINATION; IMPACT RESISTANCE; IMPACT TESTING; THERMOPLASTICS;

CARBON-FIBRE EPOXY COMPOSITES; COMPOSITE LAMINATES; COMPRESSION STRENGTH AFTER IMPACTING (CAI); DAMAGE RESISTANCE; INTERLAYER THERMOPLASTIC PARTICLES; QUASI-STATIC INDENTATION TEST (QSI); TOUGHENING MECHANISM;

LAMINATED COMPOSITES;

EID: 19044385976     PISSN: 10003851     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (15)

1. Odagiri N, Muraki T, Tobukuro K. Toughness improved high performance torayca prepreg T800H/3900 series[A]. In: Gilberto C E D, Newell W D, Brown P P, eds. Proceedings 33rd International SAMPE Symposium[C]. Covina, CA: Society for the Advancement of Material and Process Engineering, 1988. 272-283.
2. Odagiri N, Kishi H, Nakae H. T800H/3900-2 toughened epoxy prepreg system: Toughening concept and mechanism[A]. In: Proc of the 6th Conf of the American Society for Composites[C]. New Yoke: America Society for Composite, 1991. 43-52.
3. Groleau M R, Shi Y B, Yee A F, et al. Mode II fracture of composites interlayered with nylon particles[J]. Composites Science and Technology, 1996, 56(11): 1223-1240.
4. Sue H J, Jones R E, Garcia-Meitin E I. Fracture behaviour of toughened composites under mode I and mode II delamination[J]. Journal of Materials Science, 1993, 28: 6381-6391.
5. Volker A, Dale G, Michael S. Interlaminar crack growth in third-generation thermoset prepreg system[J]. Polymer, 1993, 34(4): 907-909.
6. National Materials Advisory Board. New Materials for Next-Generation Commercial Transport[M]. Washington D C: National Academy Press, 1996. 38.
7. Greenhalgh E S, Hiley M J. The assessment of novel materials and processes for the impact tolerant design of stiffened composite aerospace structures[J]. Composites Part A, 2003, 34(2): 151-161.
8. Nettles A T, Douglas M J. A comparison of quasi-static indentation to low-velocity impact[R]. NASA/TP-2000-210481. Springfield: NASA, 2000.
9. Yang X, Shen Z, Yan Y, et al. New methodology for evaluation toughness of composite laminates-investigation of damage resistance[J]. Chinese Journal of Aeronautics, 2003, 16(2): 73-79.
10. ASTM D6264-98. Standard test method for measuring the damage resistance of a fiber-reinforced polymer-matrix composite to a concentrated quasi-static indentation force[S].
11. Zhang Y Z, Ning R C. The characterizing parameters of impact resistance damage composite laminates[J]. Journal of Aeronautical Materials, 1995, 15(1): 56-62.
12. Duarte A, Herszberg I, Paton R. Impact resistance and tolerance of interleaved tape laminates[J]. Composite Structure, 1999, 47(1-4): 753-758.
13. Kageyama K, Kimpara I, Ohsawa I, et al. Mode I and mode II delamination growth of interlayer toughened carbon/epoxy (T800H/3900-2) composite system[A]. In: Martin R H, ed. Composite Materials: Fatigue and Fracture[C]. Philadelphia: American Society for Testing and Materials, 1995. 19-37.
14. Dejan S. Delamination properties of a vinyl-ester/glass fibre composite toughened by particulate-modified interlayers[D]. Canberra: Department of Engineering, Australian National University, 2001.
15. Pearson R A. Toughening Epoxies Using Rigid Thermoplastic Particles[A]. In: Keith C R, Antony J K, eds. Toughened Plastics I[C]. Washington D C; American Chemical Society, 1993.