journal article·2011-03Open access

A progressive damage simulation algorithm for GFRP composites under cyclic loading. Part I: Material constitutive model

Elias N. Eliopoulos, Theodore P. Philippidis

Composites Science and Technology· Volume 71· Issue 5

Abstract

A life prediction algorithm and its implementation for a thick-shell finite element formulation for GFRP composites under constant or variable amplitude loading is introduced in this work. It is a distributed damage model in the sense that constitutive material response is defined in terms of meso-mechanics for the unidirectional ply. The algorithm modules for non-linear material behaviour, pseudo-static loading-unloading-reloading response, constant life diagrams and strength and stiffness degradation due to cyclic loading were implemented on a robust and comprehensive experimental database for a unidirectional Glass/Epoxy ply. The model, based on property definition in the principal coordinate system of the constitutive ply, can be used, besides life prediction, to assess strength and stiffness of any multidirectional laminate after arbitrary, constant or variable amplitude multi-axial cyclic loading. Numerical predictions were corroborated satisfactorily by test data from constant amplitude fatigue of Glass/Epoxy laminates of various stacking sequences.
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Research context

OpenAlex topics: Mechanical Behavior of Composites · Structural Behavior of Reinforced Concrete · Fatigue and fracture mechanics

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (25)

Show source-provided references
1. Internal state variable approach for predicting stiffness reductions in fibrous laminated composites with matrix cracks10.1177/002199838902301205 ↗
2. Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue10.1177/002199839502900301 ↗
3. Lo DC, Coats TW, Harris CE, Allen DH. Progressive damage analysis of laminated composite (PDALC). A computational model implemented in the NASA COMET finite element code. NASA TM-4724; 1996.
4. Progressive fatigue damage modelling of composite materials. Part I: modeling10.1177/002199830003401301 ↗
5. Progressive fatigue damage modelling of composite materials. Part II: material characterization and model verification10.1177/002199830003401302 ↗
6. Failure analysis of FPF laminates by means of physically based phenomenological models10.1016/S0266-3538(96)00140-6 ↗
7. Guidelines for the determination of the parameters in Puck’s action plane strength criterion10.1016/S0266-3538(01)00202-0 ↗
8. Philippidis TP, Eliopoulos EN, Antoniou AE, Passipoularidis VA. Material model incorporating loss of strength and stiffness due to fatigue. UpWind project. Contract No.: 019945(SES6) [Deliverable 3.3.1, 2007].
9. A progressive damage mechanics algorithm for life prediction of composite materials under cyclic complex stress
10. Fatigue life prediction in composites using progressive damage modeling under block and spectrum loading10.1016/j.ijfatigue.2010.07.011 ↗
11. A progressive damage simulation algorithm for GFRP composites under cyclic loading. Part II: FE implementation and model validation10.1016/j.compscitech.2011.01.025 ↗
12. Jacobsen TK. Reference material (OPTIMAT). Glass–epoxy. OB_SC_R001_LM; 2002. .
13. Mechanical behavior of glass/epoxy tubes under combined static loading. Part II: validation of FEA progressive damage model10.1016/j.compscitech.2009.06.011 ↗
14. Megnis M, Brøndsted P. Measurements of in-plane shear properties of GEV206 at ambient room conditions using V-notched beam test specimen. OB_TG3_R009; 2003. .
15. Finite element analysis of inelastic structures10.2514/3.5125 ↗
16. Philippidis TP, Assimakopoulou TT, Antoniou AE, Passipoularidis VA. Fatigue tests on OB standard coupons at 90° Main test phase I. OB_TG2_R021; 2005. .
17. Philippidis TP, Assimakopoulou TT, Passipoularidis VA, Antoniou AE. Static and fatigue tests on ISO standard ±45° coupons Main test phase I. OB_TG2_R020; 2004. .
18. Nijssen RPL. Knowledge Centre WMC, Wieringerwerf, The Netherlands, personal communication; 2007.
19. Philippidis TP, Passipoularidis VA, Assimakopoulou TT, Antoniou AE. Fatigue tests in the fiber direction of UD OB standard specimen Main test phase I. OB_TG1_R013; 2006. .
20. Residual strength after fatigue in composites: theory vs. experiment10.1016/j.ijfatigue.2007.01.019 ↗
21. Strength degradation due to fatigue in fiber dominated glass/epoxy composites: a statistical approach10.1177/0021998308097738 ↗
22. Nijssen RPL. Fatigue life prediction and strength degradation of wind turbine rotor blade composites. PhD thesis, Faculty of aerospace engineering, T. U. Delft; 2006.
23. A study of factors affecting life prediction of composites under spectrum loading10.1016/j.ijfatigue.2008.07.010 ↗
24. Broutman LJ, Sahu S. A new theory to predict cumulative fatigue damage in fibreglass reinforced plastics. Composite materials: testing and design (2nd conference). ASTM STP 497; 1972. p. 170–88.10.1520/STP27746S ↗
25. Life prediction methodology for GFRP laminates under spectrum loading10.1016/j.compositesa.2004.02.009 ↗