Skip to main content
Disciplines
Automotive Business IT + Informatics Construction + Real Estate Electrical Engineering + Electronics Energy + Sustainability Insurance + Risk Finance + Banking Management + Leadership Marketing + Sales Mechanical Engineering + Materials
Events
DE
EN
Books
Journals
Topic Page
Marketing
Start single access now
Access for companies
EXTENDED SEARCH
Log in
Top
Applied Composite Materials
Published in: Applied Composite Materials 5/2017

19-12-2016

A Progressive Damage Model for Predicting Permanent Indentation and Impact Damage in Composite Laminates

Authors: Zhaojie Ji, Zhidong Guan, Zengshan Li

Published in: Applied Composite Materials | Issue 5/2017

Log in

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

In this paper, a progressive damage model was established on the basis of ABAQUS software for predicting permanent indentation and impact damage in composite laminates. Intralaminar and interlaminar damage was modelled based on the continuum damage mechanics (CDM) in the finite element model. For the verification of the model, low-velocity impact tests of quasi-isotropic laminates with material system of T300/5228A were conducted. Permanent indentation and impact damage of the laminates were simulated and the numerical results agree well with the experiments. It can be concluded that an obvious knee point can be identified on the curve of the indentation depth versus impact energy. Matrix cracking and delamination develops rapidly with the increasing impact energy, while considerable amount of fiber breakage only occurs when the impact energy exceeds the energy corresponding to the knee point. Predicted indentation depth after the knee point is very sensitive to the parameter μ which is proposed in this paper, and the acceptable value of this parameter is in range from 0.9 to 1.0.
previous article Micro-Mechanical Analysis About Kink Band in Carbon Fiber/Epoxy Composites Under Longitudinal Compression
next article The Use of Sprint Interface Element Delamination Simulation of Sandwich Composite Beam

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

inform now

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

inform now
Literature
1.
AC20-107B. Composite Aircraft Structures. Federal Aviation Administration, 2009. 11–14
2.
Pinho, S.T., Iannucci, L., Robinson, P.: Physically-based failure models and criteria for laminated fiber-reinforced composite with emphasis on fibre kinking. Part II: FE implementation. Comps Appl Sci Manuf 37, 767–777 (2006)
3.
Falzon, B.G., Apruzzese, P.: Numerical analysis of intralaminar failure mechanisms in composite structures. Part I: FE implementation. Compos Struct 93, 1039–1046 (2011)CrossRef
4.
Falzon, B.G., Apruzzese, P.: Numerical analysis of intralaminar failure mechanisms in composite structures. Part II: Applications. Compos Struct 93, 1047–1053 (2011)CrossRef
5.
Maimí P, Camanho PP, Mayugo JA, Dávila CG. A thermodynamically consistent damage model for advanced composites. Hampton, Virginia: Langley Research Center, National Aeronautic and Space Administration (NASA); 2006. Report No: NASA/TM-2006-214282
6.
Hashin, Z.: Failure criteria for unidirectional fiber composites. J App Mech 47, 329–334 (1980)CrossRef
7.
Puck, A., Schürmann, H.: Failure analysis of FRP laminates by means of physically based phenomenological models. Compos Sci Technol 58, 1045–1067 (1998)CrossRef
8.
Pinho ST, Dávila CG, Camanho PP, Iannucci L, Robinson P. Failure models and criteria for FRP under in-plane or three-dimensional stress states including shear non-linearity. Hampton, Virginia: Langley Research Center, National Aeronautic and Space Administration (NASA); 2005. Report No: NASA/TM-2005-213530
9.
Raimondo, L., Iannucci, L., Robinson, P., Curtis, P.T.: A progressive failure model for mesh-size-independent FE analysis of composite laminates subject to low-velocity impact damage. Compos Sci Technol 72, 624–632 (2012)CrossRef
10.
Feng, W.W., Reifsnider, K.I., Sendeckyj, G.P.: Hahn. HT. A mixed-mode fracture criterion for composite materials. J Compos Technol Res 5, 26–29 (1985)CrossRef
11.
Benzeggagh, M.L., Kenane, M.: Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus. Compos Sci Technol 56, 439–449 (1996)CrossRef
12.
Aymerich, F., Dore, F., Priolo, P.: Simulation of multiple delaminations in cross-ply composite laminates using a finite element model based on cohesive interface elements. Compos Sci Technol 69, 1699–1709 (2009)CrossRef
13.
Shi, Y., Swait, T., Soutis, C.: Modelling damage evolution in composite laminates subjected to low velocity impact. Compos Struct 94, 2902–2913 (2012)CrossRef
14.
Kim, E.H., Rim, M.S., Lee, I., Hwang, T.K.: Composite damage model based on continuum damage mechanics and low velocity impact analysis of composite plates. Compos Struct 95, 123–134 (2013)CrossRef
15.
Singh, H., Mahajan, P.: Modeling damage induced plasticity for low velocity impact simulation of three dimensional fiber reinforced composite. Compos Struct 131, 290–303 (2015)CrossRef
16.
Donadon, M.V., Iannucci, L., Falzon, B.G., Hodgkinson, J.M., Almeida, S.F.M.: A progressive failure model for composite laminates subjected to low velovity impact damage. Comput Struct 86, 1232–1252 (2008)CrossRef
17.
Feng, D., Aymerich, F.: Finite element modelling of damage induced by low-velocity impact on composite laminates. Compos Struct 108, 161–171 (2014)CrossRef
18.
Tan, W., Falzon, B.G., Chiu, L.N.S., Price, M.: Predicting low velocity impact damage and compression-after-impact (CAI) behavior of composite laminates. Comps Appl Sci Manuf 71, 212–226 (2015)CrossRef
19.
Yu, F., Chen, X., Zhang, A., Zhou, C.: Application of modified cohesive zone damage model in damage simulation of composite laminates subject to low-velocity impact. Acta Materiae Compositae Sinica 32(6), 1745–1753 (2015) [in Chinese]
20.
Choi, H.Y., Downs, R.J., Chang, F.K.: A new approach toward understanding damage mechanisms and mechanic of laminated composites due to low-velocity impact: Part I—Experiments. J Comos Mater 25, 992–1011 (1991)CrossRef
21.
Choi, H.Y., Downs, R.J., Chang, F.K.: A new approach toward understanding damage mechanisms and mechanic of laminated composites due to low-velocity impact: Part II—Analysis. J Comos Mater 25, 1012–1038 (1991)CrossRef
22.
Topac OT, Gozluklu B, Gurses E, Coker D. Experimental and computational study of the damage process in CFRP composite beams under low-velocity impact. Comps Appl Sci Manuf (2016)
23.
Fanteria, D., Longo, G., Panettieri, E.: A non-linear shear damage model to reproduce indentation caused by impacts in composite laminates. Compos Struct 111, 111–121 (2014)CrossRef
24.
Lopes, C.S., Camanho, P.P., Gürdal, Z., Maimí, P., González: Low-velocity impact damage on dispersed stacking sequence laminates. Part II: Numerical simulations. Compos Sci Technol 69, 937–947 (2009)CrossRef
25.
Faggiani, A., Falzon, B.G.: Predicting low-velocity impact damage on a stiffened composite panel. Comps Appl Sci Manuf 41, 737–749 (2010)CrossRef
26.
Bouvet, C., Rivallant, S., Barrau, J.J.: Low velocity impact modeling in composite laminates capturing permanent indentation. Compos Sci Technol 72, 1977–1988 (2012)CrossRef
27.
Hongkarnjanakul, N., Rivallant, S., Bouvet, C., Miranda, A.: Permanent indentation characterization for low-velocity impact modelling using three-point bending test. J Comos Mater 48, 2441–2454 (2014)CrossRef
28.
He, W., Guan, Z., Li, X., Liu, D.: Prediction of permanent indentation due to impact on laminated composites based on an elasto-plastic model incorporating fiber failure. Compos Struct 96, 232–242 (2013)CrossRef
29.
Hahan, H.T., Tsai, S.W.: Nonlinear elastic behavior of unidirectional composite laminae. J Comos Mater 7, 102–118 (1973)CrossRef
30.
Camanho, P.P., Dávila, C.G., Pinho, S.T., Iannucci, L., Robinson, P.: Prediction of in situ strengths and matrix cracking in composites under transverse tension and in-plane shear. Comps Appl Sci Manuf 37, 165–176 (2006)CrossRef
31.
Pinho, S.T., Darvizeh, R., Robinson, P., Schuecker, C., Camanho, P.P.: Material and structural response of polymer-matrix fibre-reinforced composites. J Comos Mater 46, 2313–2341 (2012)CrossRef
32.
Shen, Z., Yang, S., Chen, P.: Experimental study on the behavior and characterization methods of composite laminates to with stand impact. Acta Materiae Compositae Sinica 25(5), 125–133 (2008) [in Chinese]
33.
Guan, Z., He, W., Chen, J., Liu, L.: Permanent indentation and damage creation of laminates with different composite systems: an experimental investigation. Poly Mater 35, 872–883 (2014)
34.
Guan, Z., Zhao, W.: FC impact testing machine and the research of low velocity impact damage of T300/QY8911 composite plates. Acta Materiae Compositae Sinica 22, 27–31 (2005) [in Chinese]
35.
ASTM D7136/D7136M-15. Standard test method for measuring the damage resistance of a fiber-reinforced polymer matrix composite to a drop-weight impact event. West Conshohocken, PA, USA: American Society for Testing and Materials (ASTM) 2015
36.
González, E.V., Maimí, P., Camanho, P.P., Turon, A., Mayugo, G.A.: Simulation of drop-weight impact and compression after impact tests on composite laminates. Compos Struct 94, 3364–3378 (2012)CrossRef
37.
Soden, P.D., Hinton, M.J., Kaddour, A.S.: Lamina properties lay-up configurations and loading conditions for a range of fiber-reinforced composite laminates. Compos Sci Technol 58, 1011–1022 (1998)CrossRef
38.
Shoeppner, G.A., Abrate, S.: Delamination threshold loads for low velocity impact on composite laminates. Comps Appl Sci Manuf 31, 903–915 (2000)CrossRef
Metadata
Title
A Progressive Damage Model for Predicting Permanent Indentation and Impact Damage in Composite Laminates
Authors
Zhaojie Ji
Zhidong Guan
Zengshan Li
Publication date
19-12-2016
Publisher
Springer Netherlands
Published in
Applied Composite Materials / Issue 5/2017
Print ISSN: 0929-189X
Electronic ISSN: 1573-4897
DOI
https://doi.org/10.1007/s10443-016-9572-6

Other articles of this Issue 5/2017

Applied Composite Materials 5/2017 Go to the issue

OriginalPaper

Meso-Scale Damage Simulation of 3D Braided Composites under Quasi-Static Axial Tension

OriginalPaper

Tensile Properties and Failure Mechanism of 3D Woven Hollow Integrated Sandwich Composites

OriginalPaper

Spatial Evolution of the Thickness Variations over a CFRP Laminated Structure

OriginalPaper

Multi-Scale Modeling of an Integrated 3D Braided Composite with Applications to Helicopter Arm

OriginalPaper

Numerical Investigation of Thermal and Thermo-mechanical Effective Properties for Short Fibre Reinforced Composite

OriginalPaper

Fatigue Hysteresis Behavior of Unidirectional SiC/Si3N4 Composite at Elevated Temperature under Tension-Tension Loading

Premium Partners

    Image Credits