Experimental analysis of damage creation and permanent indentation on highly oriented plates

Composites Science and Technology

Volumn 69, Issue 7-8, 2009, Pages 1238-1245

  Abdallah, Elias Abi ^a   Bouvet, Christophe ^b   Rivallant, Samuel ^a   Broll, Bernhard ^a   Barrau, Jean Jacques ^b  

^a UNIVERSITÉ DE TOULOUSE   (France)

^b University of Toulouse Clement Ader Institute   (France)

Author keywords

B. Impact behaviour; B. Matrix cracking; C. Damage tolerance

Indexed keywords

B. IMPACT BEHAVIOUR; B. MATRIX CRACKING; C. DAMAGE TOLERANCE; EXPERIMENTAL ANALYSIS; EXPERIMENTAL INVESTIGATIONS; IMPACT DAMAGES; LOW-VELOCITY IMPACTS; MICROSCOPIC OBSERVATIONS; POST MORTEM ANALYSIS; QUASI-STATIC INDENTATION TESTS; STATIC AND DYNAMICS;

LAMINATED COMPOSITES; PAPER LAMINATES; REAL TIME SYSTEMS;

DAMAGE TOLERANCE;

ANALYSIS; CRACKING; DAMAGE; IMPACT; MECHANICAL PROPERTY; STRUCTURAL ANALYSIS; TESTING;

EID: 64849089979     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compscitech.2009.02.029     Document Type: Article

References (17)

1. Abrate S. Impact of composite structures (1998), Cambridge University Press, Cambridge (UK)
2. Zhang Z.Y., and Richardson M.O.W. Low velocity impact induced damage evaluation and its effect on the residual flexural properties of pultruded GRP composite. Compos Struct 81 (2007) 195-201
3. Moody RC, Harris JS, Vizzini AJ. Width effects on the compression strength of composite sandwich test specimens after barely visible impact damage. AIAA-99-1436; 1999. p. 1984-92.
4. Coutellier D., Walrick J.C., and Geoffroy P. Presentation of a methodology for delamination detection within laminated structures. Compos Sci Technol 66 (2006) 837-845
5. Alderliesten R.C. Damage tolerance of bonded aircraft structures. Int J Fatigue 1 (2008) 1-10 10.1016/j.ijfatigue.2008.05.00
6. Li C.F., Hu N., Cheng J.G., Fukumaga H., and Sekine H. Low-velocity impact-induced damage of continuous fiber-reinforced composite laminates. Part II. Verification and numerical investigation. Compos: Part A 33 (2002) 1063-1072
7. Ballère L., Viot P., Lataillade J.-L., Guillaumat L., and Cloutet S. Damage tolerance of impacted curved panels. Int J Impact Eng (2008) 10.1016/j.ijimpend.2008.03.004
8. Mitrevski T., Marshall I.H., and Thomson R. The influence of impactor shape on damage to composite laminates. Compos Struct 76 (2006) 116-122
9. Davies G.A.O., and Zhang X. Impact damage prediction in carbon composite structures. Int J Impact Eng 16 1 (1995) 149-170
10. Known Y.S., and Sankar B.V. Indentation flexure and low velocity impact damage in graphite epoxy laminates. J Compos Technol Res 15 2 (1993) 101-113
11. Kaczmarek H., and Maison S. Comparative ultrasonic analysis of damage in CFRP under static indentation and low velocity impact. Compos Sci Technol 51 (1994) 11-26
12. Sjoblom P.O., Hartness T.J., and Cordell T.M. On low velocity impact testing of composite materials. J Compos Mater 22 (1988) 30-52
13. Nettles AT, Douglas MJ. A comparison of quasi-static indentation to low velocity impact. NASA/TP-2000-210481; 2000.
14. Petit S., Bouvet C., Bergerot A., and Barrau J.J. Impact and compression after impact experimental study of a composite laminate with cork thermal shield. Compos Sci Technol 67 (2007) 3286-3299
15. Suh S.S., Han N.L., Yang J.M., and Hahn H.T. Compression behavior of stitched stiffened panel with clearly visible stiffener impact damage. Compos Struct 62 (2003) 213-221
16. Belingardi G., and Vadori R. Influence of the laminate thickness in low velocity impact behavior of composite material plate. Compos Struct 62 (2003) 27-38
17. Nettles AT, Hodge AJ. The impact response of carbon/epoxy laminates. NASA/TM-97-206317; 1997.