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Facultad de Ingeniera y Ciencias Effect of small strain rate variations on the identification of the compressive behaviour of Ti6Al4V 14 eme Colloque National en calcul des structures 13-17 mai 2019, Giens (Var), France Outline


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SLIDE 1

Effect of small strain rate variations on the identification of the compressive behaviour of Ti6Al4V

Facultad de Ingeniería y Ciencias

14 eme Colloque National en calcul des structures 13-17 mai 2019, Giens (Var), France

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SLIDE 2

Outline

2

 Introduction  Method for full range constant strain rate test  Effect of the strain rate variations on the

mechanical behavior of Ti6Al4V

 Validation of the method  Conclusions and perspectives

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SLIDE 3

3

Introduction

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SLIDE 4

4

Conventional Computer Numerical Control (CNC) milling machine

Single Point Incremental Forming for skull implant

Introduction

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SLIDE 5

Why is so important to determine and to model the mechanical behavior of metals and alloys?

5

 Design and optimization of manufacturing

processes of metals with permanent shape deformation

 e.g. sheet pile

 Estructural integrity of components

 FBO Engine test

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SLIDE 6

How to determine the mechanical behavior of metals and alloys?

6

 Mechanical tests:

 Tensile tests  Compression tests  Biaxial tests  Shear, plane strain  Etc.

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SLIDE 7

How to model the mechanical behavior

  • f Ti64 alloy or other metals?

7

Matematical formulations

Phenomenological laws

Physically based laws

 Based on micromechanics:

Slip systems, nucleation, viod growth, grain growth, etc.

 Based on macroscopic

  • bservations: load,

stress, strain, displacement fields

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SLIDE 8

8

Modeling of mechanical behavior of materials by using Finite Element Method

Material input data from experiments

Young moduli Poisson coefficients Stress strain curves Lankfords (anisotropy) Initial yield points Strain fields (DIC) Etc.

Characterization

  • f mathematical

models Simulations from Finite Element Software

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SLIDE 9

Introduction

State of the art: experimental observations

 Temperature dependent

9 Khan et al., 2004.

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SLIDE 10

Introduction

State of the art: experimental observations

 Strain rate dependent

10 Khan et al., 2004.

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SLIDE 11

Introduction

State of the art: experimental observations

 Anisotropic hardening

11

  • G. Gilles et al., 2011
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SLIDE 12

Introduction

State of the art: experimental observations

 Tension/compression asymmetry (yielding)

12

  • G. Gilles et al., 2011

Strength differential (SD) effect

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SLIDE 13

Introduction

State of the art: experimental observations

 Plastic anisotropy

13

Initial cross-section Final cross-section Notched tensile specimen

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SLIDE 14

Introduction

State of the art: constitutive modeling

 The macroscopic orthotropic yield criterion CPB06*

14

Notched tensile specimen

* Cazacu et al., 2006

     

a a a

Σ k Σ Σ k Σ Σ k Σ F

3 3 2 2 1 1 1

     

CPB06 Implemented in the Lagamine code by G. Gilles

k takes into account the strength differential effect (SD) a is the degree of homogeneity

are the principal values of the tensor is a fourth–order orthotropic tensor that accounts for the plastic anisotropy is the deviator of the Cauchy stress tensor

3 , 2 1,

   S C Σ :  C S

                    

66 55 44 33 23 13 23 22 12 13 12 11

C C C C C C C C C C C C C

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SLIDE 15

15

 Identification of the constitutive model

  • 1. Anisotropic elasto-plastic model

 Yield criterion?

Orthotropic CPB06 characterized at several plastic work levels, temperatures and at 10-3 s-1

 Hardening law?

Directional hardening: interpolation between the several yield surfaces of CPB06

 Experimental tests required for the identification:

 Tension LD (several temperatures), TD and ST directions  Compression LD (several temperatures), TD and ST directions  Plane strain LD direction (plane LD-ST)  Shear strain ST direction (plane LD-ST)

Introduction

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SLIDE 16

Outline

16

 Introduction  Method for full range constant strain rate test  Experimental results  Validation of the method  Effect of the strain rate variations on the

mechanical behavior of Ti6Al4V

 Conclusions and perspectives

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SLIDE 17

Experimental developments

Implementation of tests at constant strain rate

 Machine vs specimen deformation durinf compression test

SCHENCK Hydropuls 400 kN press

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SLIDE 18

Experimental developments

Implementation of tests at constant strain rate

18

 Tests at constant die speed (former method at MSM lab)

Displacement Time (t) Ramp

Xgl

Imposed displacement

Xgl

Time (t=t1) Time (t=tn) Time (t=0) Time (t=0) Time (t=tn)

=

Deformation of the specimen (Unknown)

Xep Xma +

Deflection of the machine (Unknown) Xgl

Time (t=t1)

Xgl

Time (t=tn)

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SLIDE 19

Experimental developments

Implementation of tests at constant strain rate

19

Deflection of the machine (test without specimen)

Load Time (t) Ramp

Xma

Time (t=t1) Time (t=0)

Xma

Time (t=t1)

Xma

Time (t=tn) Load kN Displcement Xma - mm

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SLIDE 20

Experimental developments

Implementation of tests at constant strain rate

20

 Computation of the deformation of the specimen

Deformation of the specimen is computed Xep known

Measured - test 1 Measured - test machine

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SLIDE 21

Experimental developments

Implementation of tests at constant strain rate

21

 Strain vs time computation

Strain rate is not constant Strain evolution on the specimen is computed from Xep known

   

height initial ln            H H t X H t

ep

 test at constant die speed + machine deflection forgotten

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SLIDE 22

Experimental developments

Implementation of tests at constant strain rate

 At the Time t* the machine deflection (X*

ma) is known

   

gl ma gl ma

X X X t X  ,

* 22

(for test at constant die speed)

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SLIDE 23

Experimental developments

Implementation of tests at constant strain rate

 So we can compute the deformation of the specimen (Xep)

   

) (

Test1 Test1

t X t X t X

ma gl ep

 

23

(for test at constant die speed)

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SLIDE 24

Experimental developments

Implementation of tests at constant strain rate

 Also, theoretically we know (Xep Theoretical) for constant strain rate

     

1 exp   t H t X ep  

(for a test at constant strain rate)

24

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SLIDE 25

Experimental developments

Implementation of tests at constant strain rate

25

 Globlal displacement Xgl Test 1 is computed

(for the second test at constant strain rate)

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SLIDE 26

Experimental developments

Implementation of tests at constant strain rate

26

 Comparison constant and non-constant strain rate tests

 

) speed(ramp die constant  t V

method) (new constant   

Commonly used method is wrong

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SLIDE 27

Outline

27

 Introduction  Method for full range constant strain rate test  Effect of the strain rate variations on the

mechanical behavior of Ti6Al4V

 Validation of the method  Conclusions and perspectives

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SLIDE 28

Experimental developments

Implementation of tests at constant strain rate

28

 Comparison constant and non-constant strain rate tests

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SLIDE 29

Experimental developments

Implementation of tests at constant strain rate

29

 Important for strain hardening rate

strain hardening rate

p y y

     (ramp) constant non constant      

Compression 600°C

 

y

(ramp) constant non constant      

Compression 400°C

Strain hardening rate GPa

 

y

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SLIDE 30

Outline

30

 Introduction  Method for full range constant strain rate test  Effect of the strain rate variations on the

mechanical behavior of Ti6Al4V

 Validation of the method  Conclusions and perspectives

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SLIDE 31

 Basic concept: DIC is measurement technique for full field non-

contacting deformation and strain

31

Validation of the method

Digital Image Correlation setup

Results: strain/displacement field

Calibration target

Step #2: calibration of the cameras

Loading (F)

Step #3: record images of the event Step #4: apply the correlation method Step #1: spray paint to the

  • bject (speckle pattern)

Sample

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SLIDE 32

32

Compression test

SCHENCK Hydropuls 400 kN press

Validation of the method

Digital Image Correlation setup

 3D-DIC systems configuration

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SLIDE 33

 Accurate displacement measurements and strain field computations reached

Validation of the method

Strain field by DIC measurements

Axial log. strain 33

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SLIDE 34

Experimental results at RT

Compression test for plastic anisotropy characterization

34

Why axial zz strain is not homogeneous ?

Friction effect? Plastic anisotropy? both ?

barreling

y coordinates - mm x coordinates - mm

Strain distribution at dashed line

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SLIDE 35

One-eight of the specimen is modeled

Contact elements

Why experimental axial zz strain is not homogeneous in compression tests?

 Numerical investigations of compression tests

1. Computation of Coulomb friction coefficient

ST

 1st Inverse modeling of compression for

computation of f  0.08

 Iteration fitting  Load + barreling  VM identified with compression  Verification with CPB06(4) 35

barreling is more sensitive to friction than to anisotropy

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SLIDE 36

Why experimental axial zz strain is not homogeneous in compression tests?

36

zz

horizontal centerline

 Numerical investigations of compression tests

TD ST LD LD

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SLIDE 37

Why experimental axial zz strain is not homogeneous in compression tests?

37

 Numerical investigations of compression tests

zz

Friction in compression tests influences the homogeneity

  • f the axial strain field

Material Including friction Characteristic of strain distribution Isotropic Yes Inhomogeneous No Homogeneous Anisotropic Yes Inhomogeneous No Homogeneous

(Anisotropic) (Isotropic)

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SLIDE 38

Why experimental axial zz strain is not homogeneous in compression tests?

38

 Numerical investigations of compression tests with friction

(Anisotropic) (Strongly anisotropic sheet)

Friction enhances the visualization of the plastic anisotropy through the axial strain field in compression tests

Material Characteristic

  • f

strain distribution Isotropic Weakly inhomogeneous Anisotropic Weakly inhomogeneous (different shape than isotropic) Strongly anisotropic sheet Strongly inhomogeneous

Compression sheet (stack)

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SLIDE 39

 Two ways of computing the strain:

DIC or volume conservation (Eq. 1)

Validation of the method

39

   

          ln H t X H t

ep

  • Eq. 1
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SLIDE 40

 Two ways of computing the strain:

DIC or volume conservation (Eq. 1)

Validation of the method

40

Difference caused by barreling of the sample (friction)

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SLIDE 41

Outline

41

 Introduction  Method for full range constant strain rate test  Effect of the strain rate variations on the

mechanical behavior of Ti6Al4V

 Validation of the method  Conclusions and perspectives

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SLIDE 42

Conclusions and perspectives

42

 Method for compression and tension tests at constant strain

rates using testing machine without PID control

 Validation by two method, Volume conservation and DIC

measurements at RT by measuring the full strain field of the sample during testing

 Effect of the strain rate variations on the mechanical behavior

  • f Ti6Al4V

 Mainly initial yield point  Stress hardening rate

 Axial strain sensitivity to the plastic anisotropy proposed for

inverse identification