APPLICATION ORIENTED FAILURE MODELING AND …

12
IS - Modeling of Structural Impact and Crashworthiness Application oriented failure modeling and characterization for polymers in automotive pedestrian protection XIII International Conference on Computational Plasticity. Fundamentals and Applications COMPLAS XIII H. Staack, D. Seibert and H. Baier APPLICATION ORIENTED FAILURE MODELING AND CHARACTERIZATION FOR POLYMERS IN AUTOMOTIVE PEDESTRIAN PROTECTION HOLGER STAACK *, DOMINIC SEIBERT AND HORST BAIER* * Technische Universität München - Institute of Lightweight Structures Boltzmannstraße 15, D-85748 Garching Email: [email protected] , Web page: http://www.llb.mw.tum.de AUDI AG, Ingolstadt, Germany D-85045 Ingolstadt Web page: http://www.audi.de Key words: Fracture, PC-PET, pedestrian protection, parametrization, impact testing Abstract: In the development process of automotive pedestrian protection (PedPro) for upper- and lower leg impact, the failure of polymer components plays an important role. To influence impact kinematics, fractures can either be advantageous or undesirable. Simulation based design is a challenge for material modeling and hence characterization, particularly for failure of polymer components. [1] [2] An application-oriented concept for failure modeling in FEM simulations of polymer components in pedestrian protection is presented. The boundary conditions for polymer failure in PedPro are investigated. Failure models are evaluated and selected by referring to special component tests, scanning-electron microscopy (SEM) of failure areas and simulative analysis of continuum mechanical parameters [3]. The approach of capturing the material’s behavior and consecutive modeling including parametrization is presented as well. Here a polymer blend (PC-PET) is exemplarily characterized in the highly dynamic domain. This is mainly done by using innovative pendulum tests. The parametrization of a modified Bai- Wierzbicki failure approach is performed by a numerical optimization process. The model validation is done with more complex test samples by pendulum testing. [4] [5] [6] 1 INTRODUCTION Through front vehicle design, automotive pedestrian protection reduces injuries and their aftereffects in case of vehicle-pedestrian accidents. The design is mainly based on finite element (FE) simulations. Especially for lower and upper leg impacts, fractures in polymer parts can either be desired or undesired to influence crash kinematics. However, state of the art simulation technology does not allow a reliable prediction of polymeric failure. Following, an application-oriented approach for simulative fracture in PedPro is presented. After the boundary conditions in PedPro are examined by a practice oriented component test rig, appropriate fracture modeling for polymers in PedPro is developed. During an innovative test procedure, characterization and parametrization is exemplarily performed for the polymer blend polycarbonate-polyethyleneterephtalate (PC-PET). 284

Transcript of APPLICATION ORIENTED FAILURE MODELING AND …

IS - Modeling of Structural Impact and CrashworthinessApplication oriented failure modeling and characterization for polymers in automotive pedestrian protection

XIII International Conference on Computational Plasticity. Fundamentals and Applications COMPLAS XIII

H. Staack, D. Seibert and H. Baier

APPLICATION ORIENTED FAILURE MODELING AND CHARACTERIZATION FOR POLYMERS IN AUTOMOTIVE

PEDESTRIAN PROTECTION

HOLGER STAACK*, DOMINIC SEIBERT† AND HORST BAIER* * Technische Universität München - Institute of Lightweight Structures

Boltzmannstraße 15, D-85748 Garching Email: [email protected], Web page: http://www.llb.mw.tum.de

† AUDI AG, Ingolstadt, Germany

D-85045 Ingolstadt Web page: http://www.audi.de

Key words: Fracture, PC-PET, pedestrian protection, parametrization, impact testing

Abstract: In the development process of automotive pedestrian protection (PedPro) for upper- and lower leg impact, the failure of polymer components plays an important role. To influence impact kinematics, fractures can either be advantageous or undesirable. Simulation based design is a challenge for material modeling and hence characterization, particularly for failure of polymer components. [1] [2]

An application-oriented concept for failure modeling in FEM simulations of polymer components in pedestrian protection is presented. The boundary conditions for polymer failure in PedPro are investigated. Failure models are evaluated and selected by referring to special component tests, scanning-electron microscopy (SEM) of failure areas and simulative analysis of continuum mechanical parameters [3]. The approach of capturing the material’s behavior and consecutive modeling including parametrization is presented as well. Here a polymer blend (PC-PET) is exemplarily characterized in the highly dynamic domain. This is mainly done by using innovative pendulum tests. The parametrization of a modified Bai-Wierzbicki failure approach is performed by a numerical optimization process. The model validation is done with more complex test samples by pendulum testing. [4] [5] [6] 1 INTRODUCTION

Through front vehicle design, automotive pedestrian protection reduces injuries and their aftereffects in case of vehicle-pedestrian accidents. The design is mainly based on finite element (FE) simulations. Especially for lower and upper leg impacts, fractures in polymer parts can either be desired or undesired to influence crash kinematics. However, state of the art simulation technology does not allow a reliable prediction of polymeric failure.

Following, an application-oriented approach for simulative fracture in PedPro is presented. After the boundary conditions in PedPro are examined by a practice oriented component test rig, appropriate fracture modeling for polymers in PedPro is developed.

During an innovative test procedure, characterization and parametrization is exemplarily performed for the polymer blend polycarbonate-polyethyleneterephtalate (PC-PET).

284

H. Staack, D. Seibert and H. Baier

Figure 1: Impactors used for testing in pedestrian protection [1]

2 POLYMER FRACTURE IN PEDESTRIAN PROTECTION Thermoplastic polymers show a different deformation and fracture behavior, compared to

metals, due to various molecular structure. The dependency from load conditions is therefore evident. Here, loading type and -time as well as temperature and manufacturing conditions influence the material behavior.

In PedPro, injection-molded thermoplastic components are pounded with test impactors (see Figure 1). The testing velocities reach up to 40 km/h. A comprehensive examination of material behavior in PedPro was done by Koukal [1].

2.1 Boundary conditions for modeling Modeling is constrained by the technical boundary conditions of the industrial application:

Simulations are mainly done in Pam-Crash on full-vehicle level. Model discretization is carried out with underintegrated shells with a minimum edge length of 2-4 mm. Material is modeled with elastic-viscoplastic behavior. Modeling is focused on robustness and fast applicability. (Short-)fiber-reinforced polymers are commonly simulated with homogenized fiber orientation (isotrope).

Figure 2: Front vehicle components in pedestrian protection (selection) [1]

285

H. Staack, D. Seibert and H. Baier

2.1 Polymers in pedestrian protection The material range in pedestrian protection reaches from amorphous to semicrystalline

thermoplastics, including glass-fiber reinforced polymers, polymer blends and copolymers (see Figure 2). Material and failure diversity has to be represented by the models used for simulation.

The polyesterblend PC-PET shows a notable impact strength (also under low temperature), and a good chemical resistance [7]. It is thus used as radiator grill material.

2.2 Component test rigs By full vehicle testing, a detailed examination of the fracture process is impossible. The

installation space in modern vehicles does e.g. not allow an inside installation of high speed camera systems. Hence, a component test rig was designed in order to examine polymer failure under realistic test conditions. The test rig reduces the number of parts to 3 (cf. Figure 3). At least, the vehicle behavior is simulated in a realistic manner [3]. For testing, the PDI-1 sensoric impactor (9,8 kg) is blasted at the installation with 20-25km/h. By shooting at different positions, fractures in all parts can be triggered. The tests were con-ducted and monitored in an overall 50ms time frame.

Additional to fracture examination, the rig tests can be used for fracture model validation.

Figure 3: Component test rig used for fracture study and model validation [3]

2.3 Common and specific boundary conditions for polymeric failure Boundary conditions for fracture are examined during experiments and the corresponding

simulation. Strain and strain rates in fractured areas could be determined to be bound in-between 100 and 102 1/s (strain rates) and 10-1 up to 101 (strain).

The stress triaxiality is defined to be the quotient of the mean or hydrostatic stress σm and the equivalent Von-Mises stress σequ (cf. equation 1). Within the failing zone, triaxialities could be determined between and for shell elements. Failure at pure shear state or at negative triaxialities could not be examined.

The areas with a high failure risk are mostly ribbed and are complex geometries, that lead

286

H. Staack, D. Seibert and H. Baier

to a higher triaxiality. Figure 4 shows a triaxiality curve typical for failing elements in PedPro simulations. (1)

Figure 4: Typical stress triaxiality (at upper, mid and lower integration point of shell a element) during testing in PedPro, exemplarily for a selected element in the grill stiffener

Koukal und Delhaye verified a volume increase for polypropylene (PP), polyethylene (PE) and polyvinylchloride (PVC). This effect increases with increasing strain rate. [1] [8] Fracture at tensile tests occurs normal to load direction.

Examination of fracture areas from the tested components with the scanning-electron

microscope (SEM) verify the tendency of fracture: Independent of the plasticity of material, the fracture area seems consistently to be quasi-brittle. However, on molecular level, indications for plastic deformation (crazing) before fracture can be found (see Figure 5). Only the behavior of talcum reinforced PP is purely brittle.

Crazing is mainly known to be characteristic for amorphous polymers and their blends. As

can be seen from the SEM results, also the semicrystalline thermoplastics show marks for crazing (see Figure 5).

Failure during pressure tests could only be examined under large deformation of polymer samples. Due to the surface deformation, the areas of initial fracture are not pressure-dominated. During shear tests, ductile thermoplastics displayed a tendency for failure in tensile-dominated areas. Failure due to pure pressure is thus considered to be impossible. Shear failure is at least theoretically possible. A good theoretical overview of polymeric failure mechanisms is given by Michler and Baltá-Calleja [9].

287

H. Staack, D. Seibert and H. Baier

Figure 5: SEM pictures of fracture areas from impact tests on component test rig. Top left to bottom right:

talcum-filled polypropoylene (PP-T40), long-glassfiber-reinforced polypropylene (PP-LGF30), polycarbonate-polyethyleneterephtalate (PC-PET), glassfiber-reinforced polyamide (PA6-GF30) [3]

Boundary conditions for failure are summarized as follows:

Low-deformation plastic fracture due to crazing Triaxiality at failure Strong dependency on strain rate and triaxiality

2.4 Fracture models Failure modeling for PedPro has to consider these constraints. Simple criteria, like

maximum plastic strain, neglect e.g. the influence of stress conditions. Therefore, the stress triaxiality has to be taken into account as well as the strain rate influence on the deformation behavior. If using shell elements for simulation, the Lode parameter can be neglected as fracture parameter, since a plane stress condition can be postulated [10]. For volume elements, the Lode parameter has to be considered.

Analog to the examination of Bao [11] and Greve [12], failure due to pure pressure is excluded. Hence, a cut-off-value at is necessary for fracture modeling. Considering the results of Koukal [1], fracture strain is assumed to be decreasing with increasing triaxiality and strain rate (cf. equation 2 and 3)

288

289

H. Staack, D. Seibert and H. Baier

3-point-bending tests (c3PB) are loaded quasistatic and dynamic until fracture occurs (see Figure 6/4). Additionally, tensile tests are performed. For data sets close to , puncture tests on clamped plates are evaluated (see Figure 6/3). For validation purpose, dynamic and quasistatic 3-point-bending tests (3PB) with T-samples (cf. Figure 6/5) are used in addition to component tests (see 2.2).

Figure 6: Portfolio of material tests used for material characterization [6]

2.6 Parametrization of the fracture model The fracture parameters are derived by the help of simulation with a validated material

model. For this purpose, plastic strain rate and stress triaxiality for the failing area during testing is averaged over the deformation. For the resultant data pair, the plastic strain is determined. Averaging of is done due to Bao-Wierzbicki [18] (cf. equation 7).

(7)

Figure 7: Averaging of the stress triaxiality in the plastic region, exemplarily for the clamped 3-point-bending test. Simulation is diagramed as quarter model

290

H. Staack, D. Seibert and H. Baier

Analogously, the plasti is averaged (equation 8).

(8)

The data points at low strain rates are used to calibrate the parameters D1-D3 in 2D ), before the strain rate parameter D4 is adopted by the help of dynamic data points. In case of data points at different strain rates and triaxialities, the parameter fitting is done in 3D ) for all parameters at the same time (cf. Figure 8).

3 RESULTS

3.1 Experimental data

From the experiments described in 2.5, the data points parametrization (see Table 1).

-

3.2 Parametrization For numerical optimization of the failure model‘s weighting function εfail, gradient based

algorithms are used by an inhouse Matlab tool [19]. Least square is used to set up the objective function. Figure 8 shows a exemplary data set with convenient test settings for the Johnson-Cook criterion [16].

The optimization with the data points presented in Table 1 results in following fracture parameters for the simplified mBW fracture model:

The resultant failure area is illustrated in Figure 9, together with performed tests for characterization and used data points.

291

H. Staack, D. Seibert and H. Baier

Figure 8: Example for ideal points for a 2D optimization with separate strain-rate dependency, plotted for the Johnson-Cook fracture model

Figure 9: Optimized failure area for the mBW fracture model, parametrized for PC-PET with the data points presented in Table 1

3.1 Validation For the first validation steps, the tests conducted for parametrization were used (cf. 2.5).

Thereafter, the T-specimen are used for validation close to component. The load case represented by the T-specimen is typical for ribbed injection molding components in PedPro

292

H. Staack, D. Seibert and H. Baier

testing situations (cf. Figure 1). The simulation results show a good correlation with the test data for c3PB (Figure 10) as well as for the T-specimen (Figure 11).

Figure 10: Comparison of test and simulation results (5 tests averaged, 4 m/s) of pendulum force over time, with failure for a clamped 3-point-bending test

4 DISCUSSION The presented fracture model shows a good correlation with experimental data for

PC-PET. For the c3PB tests, a good repeatability of failure can be noted. The simulated sample shows a similar load-displacement characteristic and a similar initial failure (cf. Figure 10). The conducted validation revealed that the imposed failure model is capable of predicting failure location as well as time of occurrence (cf. Figure 11).

The adaption of the plastic model is not fully finished for the complete triaxiality range, being . Thus, the material model with the Raghava plasticity (see 2.4) does not represent the biaxial behavior with sufficient accuracy. The validation of the biaxial puncture tests has to be repeated with an adapted plastic model, to reach a satisfactory simulation quality.

The test results show an increase in failure strain for high triaxialities. This behavior

cannot be represented by the Johnson-Cook approach (see Figure 8 and equation 9) [16], whereas the simplified mBW model allows this increase.

(9)

Averaging of triaxiality and strain rate seems to be feasible due to the good test quality and the linear damage accumulation approach (cf. [12]).

To improve the model quality for failure and to confirm the complex material behavior of PC-PET, more data points have to be generated. Herein, dynamic tensile- and shear tests will be carried out as well as notched tensile tests. The data points for fracture are now derived by a method, that depends on fracture times.

293

H. Staack, D. Seibert and H. Baier

If the material model does not completely correlate with the physical behavior of the material, the data point extraction is not correct.

The strain rate dependency on only one parameter, as adapted from the Johnson-Cook criterion, should be verified for PC-PET. Here, the independency from the stress triaxiality level has to be verified. However, to fit the strain rate dependency with certainty, 3 different data points at one triaxiality level have to be created.

Figure 11: Comparison of test and simulation results (5 tests averaged, 4 m/s) of pendulum force over displacement, with failure for a 3-point-bending test with T-specimen. Upper left: Simulation close to fracture

(half model). Lower left: T-specimen after testing

5 CONCLUSIONS Through the characteristic of increasing failure strains at high triaxialities and the coupled

strain rate dependency from Johnson-Cook, the simplified mBW model (simplified for plane stress) is a good alternative to complex fracture criterions like Crach-FEM [20]. Due to the included asymptote at , compression testing is dispensable.

The experimental characterization of polymer fracture for parametrization with Impetus pendulum tests is easy to adapt and the results are promising. Through the semi-automated testing- and parametrization process, the step from model to industrial application becomes shorter compared to conventional testing. The analysis of the application’s scope allows the usage of a straight forward implemented models for a complex application.

Validation tests on sample level show a good correlation of simulation and testing. Fracture location and time can be predicted in a more reliable way, compared to former models [1].

For high triaxialities, material modeling has to be improved (cf. 4). Further validation with component tests (cf. 2.5) will be done to prove the adaptability of the method to practical industrial problems.

Finally, the described characterization process will be performed for further polymers, in order to use the advantages of the method in a multi-material front vehicle (cf. Figure 2).

294

H. Staack, D. Seibert and H. Baier

REFERENCES [1] A. Koukal, “Crash- und Bruchverhalten von Kunststoffen im Fußgängerschutz von

Fahrzeugen,” TU München, 2014. [2] D. Seibert and H. Staack, “On the virtual development of pedestrian protection,” in

International Conference Intelligent Collision Protection and Pedestrian Protection, 2014. [3] H. Staack, D. Seibert, A. Koukal, and H. Baier, “Versuchsbasierte Entwicklung eines

industriellen Bruchkriteriums für Kunststoffkomponenten in der Fußgängerschutzauslegung,” in SIMVEC, 2014.

[4] H. Staack, “Charakterisierung von (kurzfaserverstärkten) Kunststoffen für die Crashsimulation beim Fußgängerschutz,” in Hochleistungsstrukturen im Leichtbau, 2014.

[5] P. Reithofer, M. Rollant, and A. Fertschej, “Anpassung komplexer Fließflächen und Möglichkeiten der Versagensabbildung mit 4a Impetus,” in Dynamore Infotag Kunststoffe, 2013.

[6] A. Fertschej, P. Reithofer, and M. Rollant, “Versagen von Thermoplasten - Charakterisierung, Versuche,” in DYNAFORUM 2014, 2014.

[7] E. Baur, S. Brinkmann, T. Osswald, N. Rudolph, and E. Schmachtenberg, Saechtling Kunststoff Taschenbuch, 31st ed. Hanser Verlag, 2013.

[8] V. Delhaye, “Behaviour and modelling of polymer for crash applications,” NTNU Trondheim, 2010.

[9] G. H. Michler and F. J. Baltá-Calleja, Nano- and Micromechanics of Polymers. München: Carl Hanser Verlag, 2012.

[10] Y. Bai and T. Wierzbicki, “A comparative study of three groups of ductile fracture models,” Eng. Fract. Mech., pp. 1–31, 2015.

[11] Y. Bao and T. Wierzbicki, “On the cut-off value of negative triaxiality for fracture,” Eng. Fract. Mech., vol. 72, no. 7, pp. 1049–1069, 2005.

[12] L. Greve, “Advances in Fracture Modeling for Crash Simulation Using the Multi-model Coupling Method,” VDI Berichte, vol. 2031, pp. 587–601, 2008.

[13] S. Hayashi, “Prediction of Failure Behaviors in Polymers Under Multiaxial Stress State,” in 12th International LS-DYNA Conference, no. 3, pp. 1–14.

[14] S. Lin, Y. Xia, C. Lin, J. Wang, and G. Gu, “Stress State Dependent Failure Loci of a Talc-filled Polypropylene Material under Static Loading and Dynamic Loading,” in 13th International Conference on Fracture, 2013, vol. 1, no. 1, pp. 1–16.

[15] Y. Bai and T. Wierzbicki, “A new model of metal plasticity and fracture with pressure and Lode dependence,” Int. J. Plast., vol. 24, no. 6, pp. 1071–1096, Jun. 2008.

[16] C. W. H. Johnson G.R., “Fracture characteristics of three metals subjected to various strains, strain rates, temperatures and pressures,” Eng. Fract. Mech., 1985.

[17] R. Raghava, R. M. Caddell, and G. S. Y. Yeh, “The macroscopic yield behaviour of polymers,” J. Mater. Sci., vol. 8, no. 2, pp. 225–232, 1973.

[18] Y. Bao and T. Wierzbicki, “On fracture locus in the equivalent strain and stress triaxiality space,” Int. J. Mech. Sci., vol. 46, pp. 81–98, 2004.

[19] P. Eiperle, “Numerical optimization of fracture models for crash simulation in pedestrian protection,” TU München, 2015.

[20] H. Werner, H. Hooputra, H. Dell, and H. Gese, “A phenomenological failure model for sheet metals and extrusions,” in Annual review meeting and workshop of Impact and Crashworthiness Lab at MIT, 2004.

295