Analytical Prediction of Springback, sheet metal forming

7/31/2019 Analytical Prediction of Springback, sheet metal forming

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Analytical prediction of springback based on residualdifferential strain during sheet metal bendingH K Yi1, D W Kim1, C J Van Tyne2, and Y H Moon1*1Engineering Research Center for Net Shape and Die Manufacturing/Department of Mechanical Engineering, Pusan

National University, Busan, Republic of Korea2Department of Metallurgical and Materials Engineering, Colorado School of Mines, Golden, Colorado, USA

The manuscript was received on 30 March 2007 and was accepted after revision for publication on 11 September 2007.

DOI: 10.1243/09544062JMES682

Abstract:As the springback of sheet metal during unloading may cause deviation from a desiredshape, accurately predicting springback is essential for the design of sheet stamping operations.Finite-element models have not been successful in predicting springback; hence there is a needfor analytical models to make such predictions. In this study, a model based on differentialstrains after relief from the maximum bending stress is derived for six different deformation pat-terns in order to predict springback analytically. The springback for each deformation pattern isestimated by the residual differential strains between outer and inner surfaces after elasticrecovery. Each of the six deformation patterns has a valid region of applicability, based on elas-tic modulus, yield strength, applied tension, and bending geometry. Analytical equations for thespringback of the sheet deformed under these six deformation patterns are derived. Traditionalanalytical models for springback prediction have been based on elastic unloading from a bend-ing moment. Traditional models also require the knowledge of the stress distribution through

the thickness of the sheet, whereas the residual differential strain model only requires thestress state on the outer and inner surfaces of the sheet. In order to compare the residual differ-ential strain model with the traditional bending moment model, a bending moment model isderived for the same exact deformation patterns. Results from the two models are comparedfor various materials.

Keywords: springback, sheet metal forming, analytical model, residual differential strain,bending moment model, multiple deformation patterns

1 INTRODUCTION

Springback refers to the elastic recovery of deformedparts. Springback occurs because of the elastic relieffrom the bending moment imparted to the sheetmetal during forming. Springback is common andinevitable in each stage of the production process

where the material undergoes geometrical changes.Accordingly, factors related to the generation ofstress in the material during loading and unloading

processes influence the springback behaviour ofpress-formed parts [14].

The application of high strength steels and alu-minium to automotive sheet components is increas-ing, as they effectively reduce body weight whilekeeping and improving structural performance [5,6]. Unfortunately, these materials tend to have alarger springback than mild steels. The high valuesof the ratio of strength to Youngs modulus result inmore springback. For a given amount of deformation,higher strength materials (e.g. high strength steels)

will unload from a higher strength, resulting inmore elastic unloading strain. Likewise, for a material

with a lower Youngs modulus (e.g. aluminium

alloys), the amount of elastic unloading strain,which causes the springback, is higher. Overall, it is

*Corresponding author: Engineering Research Center for Net

Shape and Die Manufacturing, Department of Mechanical Engin-

eering, Pusan National University, San 30, Jangjeon-dong,

Geumjeong-gu, Busan 609-735, Republic of Korea. email:[email protected]

117


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more difficult to accurately produce a part shapewithout proper springback compensation. As spring-back is strongly dependent on the part geometry andthe materials used, it is not possible to give a generalrule of thumb for its compensation. Commercialfinite-element programme for sheet forming simu-lation give good results in terms of formability,strain distribution, and wrinkling but springbackremains a phenomenon often reported as being diffi-cult to simulate. There are certain aspects that makespringback especially critical for sheet metal forming[610]. Even small angular springback in deep drawnstructures may cause large spatial deformations anddistortions of the whole part. As finite-element simu-lations are computationally intense, efficient analyti-cal methods to predict springback have also beendeveloped [11 13].

In this study, a model based on differential strains

after relief from the maximum bending stress [14,15] is derived for multiple deformation patterns (i.e.different stress conditions) in order to predict spring-back analytically. The springback for each defor-mation pattern is estimated by the residualdifferential strains between outer and inner surfacesafter elastic recovery. As the springback of sheetmetal after bending is strongly dependent on thestress state of the deformed sheet, six different defor-mation patterns, each having a valid region ofapplicability, are derived on the basis of material par-ameters (elastic modulus and yield strength), applied

tension, and bending geometry. Analytical equationsfor the springback of the sheet deformed under thesesix deformation patterns are derived.

Traditional analytical models for springback pre-diction have been based on elastic unloading from abending moment [13, 16]. Such models are morecomplicated than the residual differential strainmodel that is derived in the present study. Traditionalmodels also require the knowledge of the stressdistribution within the part under examination,

whereas the residual differential strain model onlyrequires the stress state on the outer and innersurfaces of the sheet. In order to compare the residualdifferential strain model with the traditionalbending moment model, a bending moment modelis derived for the same exact deformation patterns.Results from the two models are compared for var-ious materials.

2 ANALYTICAL MODELS FOR SPRINGBACKPREDICTION

Consider the bending process as shown in Fig. 1,

where a unit width of a continuous sheet is bent toa radius of curvature r, and the bend angle is u.

Moment per unit width, M, and tension (force perunit width), T, are applied to the sheet. When thesheet is bent by a pure moment without any tensionbeing applied, the neutral axis will be at the mid-

thickness of the sheet. The upper half thicknessabove neutral axis will be in a tensile stress state,

whereas the lower half thickness is in a compressivestress state. In pure bending, the maximum strainoccurs in the outer (upper) surface, and the elasticplastic behaviour at this region is determined by thematerial parameters (elastic modulus E and yieldstrength so) and bending geometry. The strain atthe yield point 1o is

1o so

E1

and the maximum strain applied on the outer surface1max can be expressed by

1max t

2r2

where tis the thickness of the sheet and ris the radiusof the bend.

When 1max exceeds 1o, then the outer surface willbe in a plastic stress state, but if the reverse is true,then the outer surface will be in an elastic stressstate. As the springback of sheet metal after bending

is strongly dependent on the stress state of thedeformed sheet, the springback parameter Sp is intro-duced for the precise classification of deformationbehaviour by dividing equation (2) by equation (1)to obtain

Sp 1max

1o

Et

2rso3

when Sp is greater than 1, the outer surface will be in aplastic stress state and when Sp is less than 1, theouter surface is in an elastic stress state. Figure 2

schematically shows the classification of the spring-back parameter.

Fig. 1 A unit length of a continuous strip bent along a

line

118 H K Yi, D W Kim, C J Van Tyne, and Y H Moon


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If the desired curvature of a sheet is less than thelimiting elastic curvature, the sheet cannot beformed to shape simply by bending over a dieblock. It would either springback to the flat shape,or if it were over-bent until it becomes partially plas-tic, the springback would be so high that the process

would be difficult to control. Therefore, in a stampingoperation, tension is frequently applied to the sheet,

which is first curved elastically to the shape of a dieblock. For such conditions, the initial moment andthe stress state will be changed because of the appli-

cation of tension.In the current study, the possible variations of

stress states for bent sheet with applied tension areclassified on the basis of the amount of the appliedstrain, 1a, which originates from applied stress, sa.

When Sp is less than one, three different deformationpatterns are possible, as shown in Table 1 and Fig. 3.

When Sp is greater than one, three different defor-mation patterns can occur, as shown in Table 2 andFig. 4. Therefore, six different analytical models arederived one for each deformation pattern. Fromthe given process conditions and material par-

ameters, the valid deformation pattern is determinedfirst and then the amount of springback can becalculated.

2.1 Springback model based on residual

differential strainTo date, most analytical springback models havebeen based on elastic recovery from the appliedbending moment that causes the bend. This type oftraditional model will be derived in section 2.2. Inthis section, a model based on the residual differen-tial strain is derived. Differential strain is the differ-ence between the strain on the outer surface of thebend and that on the inner surface of the bend. Theresidual differential strain method produces simpleranalytical equations to determine springback frombending. In addition, the method only requires

knowledge of the stress state on the outer and innersurfaces of the bend, rather than the stress distri-bution through the thickness of the sheet.

Consider the case of a sheet metal bent to radius rby applying uniform bending moment. If r is suchthat the maximum stress induced lies within the elas-tic limit of the material, then on removing the bend-ing moment, the specimen will return to the originalshape. However, ifris such that the maximum stressinduced exceeds the elastic limit of the material, plas-tic strain will occur at the outer surface and thematerial will take a permanent set. If on removal of

the bending moment, the elastic unloading of thematerial is not uniform across the thickness, thenspringback will occur. The bend radius rwill not be

Fig. 2 Classification of springback parameter (Sp)

Table 1 Three possible deformation patterns for Sp41

(i.e. s0/E5 t/2r)

Innersurface

Outersurface Valid range ID

Elastic Elastic 1a2 t/2r52s0/E, 1a t/2r4s0/E) 041a4s0/E2 t/2r

SA

Elastic Plastic 1a2 t/2r4s0/E, 1a t/2r5s0/E) s0/E2 t/2r41a4s0/E t/2r

SB

Plastic Plastic 1a2

t/2r5s0/E, 1a t/2r5s0/E) 1a5s0/E t/2rSC

Fig. 3 Possible deformation for given deformation

patterns for SP41

Table 2 Three possible deformation patterns for Sp51

(i.e. t/2r5s0/E)

Innersurface

Outersurface Valid range ID

Plastic Plastic 1a2 t/2r42 s0/E,1a t/2r5s0/E) 041a4 t/2r2 s0/E

LA

Elastic Plastic 1a2 t/2r52s0/E,1a t/2r5s0/E) t/2r2 s0/E41a4 t/2r s0/E

LB

Plastic Plastic1a2

t/2r5

s0/E,1a t/2r

5s0/E) 1a5 t/2r s0/E LC

Analytical prediction of springback 119


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maintained in the sheet. Consider a similar specimenthat is bent over a rigidly supported die of cylindricalcross-section of radius r with a tensile load beingapplied to each end of the specimen. The tensilestress due to bending is increased and the compres-sive stress is decreased. As the applied load isincreased, the compressive stress is decreasedfurther, and eventually the whole specimen is in ten-sion to a varying degree. Moreover, if the stress on theouter surface (i.e. the surface with the greatest radius)exceeds the elastic limit of the material, the increasedapplied tension will cause the load to be more evenly

distributed throughout the thickness of the material.Eventually, a level of applied load is reached wherethe stress in the specimen is nearly uniform and theentire sheet thickness is in the plastic range. Remov-ing the applied load, the specimen loses its elasticstrain by contracting, and the final radius in thebent sheet can be determined from the residualdifferential strain.

The springback, SB, for each deformation pattern isestimated by the residual differential strains betweenouter and inner surfaces of greatest radius after elas-tic recovery as

SB 1l 1u

1l4

where 1l is the strain difference between outer andinner surfaces of greatest radius while loaded and 1uis the strain difference between outer and inner sur-faces of greatest radius after unloading. Because themodel is based on residual differential strains in thesheet, springback is defined in terms of strain ratherthan the traditional measure of angular change.

Figure 5 shows the deformation pattern for SA inwhich both the inner and outer surfaces are elastic,

and the resulting springback is given by

SB 1l 1u

1l1l 0

1l 1:0 100% 5

Figure 6 shows the deformation pattern for SBwhere the inner surface is elastic, whereas the outersurface is plastic, and the resulting springback isgiven by

SB 1l 1u

1l1l 1a t/2r sun/Eun

1l6

where Eun is the unloading modulus, 1a the appliedaxial strain, and sun the strength of the sheet materialprior to unloading.

As 1l 1b t/r, where 1b is the bending strain, then

SB t 2rsun/Eun 1a

2t7

Fig. 4 Possible deformation for given deformation

patterns for SP51

Fig. 6 Stressstrain distribution for deformationpattern SB

Fig. 5 Stressstrain distribution for deformation

pattern SA



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The strength of the sheet can be modelled as apower law type of material, so that sun K(t/2r1a)

n, where K is the strength coefficient of the sheetmaterial and n is the strain hardening exponent forthe sheet material.

Figure 7 shows the deformation pattern for SC,where both inner and outer surfaces are plastic andthe amount of springback is

SB 1l 1u

1l

t/r 1a t/2r K1a t/2rn=Eu1

1a t/2r K1a t=2rn/Eu21l

Kr1a t/2r

n/Eu1 1a t/2rn/Eu2

t8

where Eu1 and Eu2 are the unloading moduli form theouter and inner surfaces, respectively.

Figure 8 shows the deformation pattern for LA,where both inner and outer surfaces are plastic, andassuming that Eu1 Eu2 Eun, the amount of spring-back is

SB 1l 1u

1l

su1/Eu1 su2/Eu21l

Kt/2r 1a

n Kt/2r 1an

t/r Eun

Krt/2r 1a

n t/2r 1an

tEun9

where the strength of the sheet on the outer surface issu1 K(t/2r 1a)

n and the strength of the sheet onthe inner surface is su2 2K(t/2r2 1a)

n.

Figure 9 shows the deformation pattern for LB,where the inner surface is elastic and the outer

surface is plastic, and the amount of springback is

SB 1l 1u

1l1l 1a t/2r sun/Eun

1l10

as 1l 1b t/r, therefore

SB t 2rsun/Eun 1a

2t11

where sun K(t/2r 1a)n

Figure 10 shows the deformation pattern for LC,where both inner and outer surfaces are plastic and

Fig. 7 Stressstrain distribution for deformation

pattern SC

Fig. 8 Stressstrain distribution for deformationpattern LA

Fig. 9 Stressstrain distribution for deformationpattern LB



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the amount of springback is

SB 1l 1u

1l

t/r 1a t/2r K1a t/2rn/Eu1

1a t/2r K1a t=2rn/Eu2

1l

Kr1a t/2r

n/Eu1 1a t/2rn/Eu2

t12

2.2 Springback model based on bending moment

To compare the residual differential strain modelderived in the previous section, a second analyticalmodel based on the bending moment [14, 15] isderived for the same six deformation patterns. Thebending moment model is the traditional analyticalmodel used to determine springback. The bendingmoment model depends on the unloading from anapplied moment in the sheet, causing a change inthe curvature of the bend.

When a normal section of unit width of the sheet is

bent, a stress distribution due to bending occurs.Tension, T, on the sheet causes a change in thestress distribution, such that T will balance the inte-gral of the stress distribution due to static equili-brium. The bending moment can be obtained byfinding the first moment of the stress distribution.By examining analytical expressions for the tension,T, and the bending moment, M, the springback canbe obtained.

From the moment at a given condition beforeunloading

Ms I E 1r

13

where subscript s indicates the start of the unloadingprocess, I the moment of inertia and 1/r the curva-ture in the sheet caused by the moment.

rwill change as the moment changes, so

DM I E D 1r

14

Extraction of the sheet from a die means Mf 0,where the subscript f indicates the finish of theunloading process. Therefore, during unloading

DM Mf Ms 0 Ms Ms 15

The change in the bending radius is

D

1

r

1

r

f

1

r

sDM

I E Ms

I E Du 16

where Du, the angular change, is the measure of thespringback.

For a rectangular sheet cross-section, the momentof inertia per unit width (i.e. w 1) is

I wt3

12

t3

1217

Therefore

Du D1

r

1

r

f

1

r

s

12 Ms

E t318

Figure 11 shows the deformation pattern for SAwhere both inner and outer surfaces are elastic.

Tension Tfor the deformation pattern for SA is

T

t=2t=2

E

r

2a 1

2

t

E

r y

dy

E2a 1 t2

2r19

Fig. 10 Stress strain distribution for deformation

pattern LC

Fig. 11 Stress distribution for deformation pattern SA



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where, for this deformation pattern, a is the normal-ized distance between the outer surface of the sheetand the neutral plane.

Moment, M, for the deformation pattern SA is

M t=2

t=2

Er

2a 12

t E

r y

y dy

E

3r

t3

8

t3

8

E t3

12r20

From equation (16), the springback is

SB 1/rs 1/rf

1/rs

12M

1/rsEt3

21

Note that equation (21) is a different equation for

springback when compared with the definitiongiven in the residual differential strain model inequation (4). The difference is due to the fact thatthe traditional bending moment model relies on themomentcurvature relationship and defines spring-back in terms of angular change as in equation (16).

As the springback measure for both models is deter-mined on a percentage basis and both modelsaccount for the elastic unloading after bending, acomparison between the two models can be madedespite the differences between the two definitions.

Figure 12 shows the deformation pattern for SB,

where the inner surface is elastic and the outer sur-face is plastic.

Tension Tfor the deformation pattern for SB is

T

t=2t=2at

s dy1

2 s20

r

E

1

2s0

E b t

r

bts0 r

E

r K

n 1

t

2r1a

n1

1 2a t

2r1a

n1( )

E b2

t2

2rs0 b t 22

where, for this deformation pattern, a is the normal-ized distance between the outer surface and the planein the sheet at the yield strength and b is the normal-ized distance between the plane in the sheet at the

yield strength and the bottom surface. In this case,a b 1.

Moment M for the deformation pattern for SB is

M

t=21=2at

sy dy

1=2att=2

E

rys0

2b 1

2

t E

r

y dy

Kr2

n2

t

2r1a

n2

1 2a t

2r1a

n2( )

Kr2 1a

n 1

t

2r1

a n1

1 2a t

2r 1

a n1( )

E

3r

1 2a

2

3 t3

t3

8

" #s0

2

12a

2

2 t2

t2

4

" #

2b 1

4

E t

r

1 2a

2

2 t2

t2

4

" #23

From equation (18), the springback is

SB 1/rs 1/rf

1/rs

12M

1/rsEt324

Figure 13 shows the deformation pattern for SC,where both the inner and outer surfaces are plastic.

Tension T for the deformation pattern for SC is

T

t=2t=2

s dy

t=2t=2

K y

r 1a

n dy

r K

n 1

t

2r 1a

n1

t

2r 1a

n1" #25

Fig. 12 Stress distribution for deformation pattern SB Fig. 13 Stress distribution for deformation pattern SC



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Moment Mfor the deformation pattern for SC is

M

t=2t=2

s y dy

t=2t=2

K y

r 1a

ny dy

r2 Kn 2

t2r

1a

n2

t2r

1a

n2

" #

r2 K

n 1

t

2r 1a

n1

t

2r 1a

n1" #

26

The springback can be obtained from equation (24).Figure 14 shows the deformation pattern for

LA, where both the inner and outer surfaces areplastic.

Tension Tfor the deformation pattern for LA is

T

t=2t=2at

s dy1

4s0 b t

1

4s0 b t

t=22a2b1=2t

s dy

r K

n 1

t

2r 1a

n1

1 2a t

2r 1a

n1( )

r K

n 1

t

2r1

a n1(

2a 2b 1 t

2r 1a

n1)27

where, for this deformation pattern, a is the normal-ized distance between the outer surface and the planein the sheet at the yield strength and b is the normal-ized distance between the first plane in the sheet atthe yield strength and the second plane in the sheetat the yield strength.

Moment Mfor the deformation pattern for LA is

Mt=2

12a=2tsy dy

12a=2t12a2b=2t

2 s0 y

bt

s0b2a1

b

y dy

t=212a2b=2t

sy dy

r2 K

n2

t

2r1a

n2

12at

2r1a

n2( )

Kr2 1a

n1

t

2r1a

n1

12at

2r1a

n1( )

2 s0

3 bt

1

2

a 3

t3 s0 b2a1

2b

12a

2

2

t2

2 s03 bt

1

2ab

3 t3

s0b2a1

2b

12a2b

2

2 t2

r2 K

n2

t

2r 1a

n2

2a2b1t

2r1a

n2( )

Kr2 1a

n1

t

2r1a

n1(

2a2b1 t

2r1a

n1)28

The springback can be obtained from equation(24).

Figure 15 shows the deformation pattern for LB,where the inner surface is elastic and the outersurface is plastic.

Fig. 14 Stress distribution for deformation pattern LA Fig. 15 Stress distribution for deformation pattern LB



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Tension, T for the deformation pattern for LB is

T

t=2t=2at

s dy1

2 s20

r

E

1

2s0

E b t

r

bts0 r

E

r K

n 1

t

2r 1a

n1

1 2a t

2r 1a

n1( )

E b2 t2

2r s0 b t 29

where, for this deformation pattern, a is the normal-ized distance between the outer surface and the planein the sheet at the yield strength and b is the normal-ized distance between the plane in the sheet at the

yield strength and the bottom surface. In this case,a b 1.

Moment Mfor the deformation pattern for LB is:

M

t=21=2at

sy dy

1=2att=2

E

rys0

2b 1

2

t E

r

y dy

K r2

n 2

t

2r 1a

n2

1 2a t

2r 1a

n2( )

K r2 1a

n 1

t

2r 1a

n1

1 2a t

2r 1a

n1( )

E

3r

1 2a

2

3 t3

t3

8

" #

s0

2

1 2a

2

2 t2

t2

4

" #

2b 1

4

E t

r

1 2a

2

2 t2

t2

4

" #30

The springback can be obtained from equation(24).

Figure 16 shows the deformation pattern for LC,where both inner and outer surfaces are plastic.

Tension Tfor the deformation pattern for LC is:

T

t=2t=2

s dy

t=2t=2

K y

r 1a

n dy

r K

n 1

t

2r 1a

n1

t

2r 1a

n1

" # 31

Moment M for the deformation pattern for LC is

M

t=2t=2

s y dy

t=2t=2

K y

r 1a

ny dy

r2 K

n 2

t

2r

1a n2

t

2r

1a n2

" #

r2 K

n 1

t

2r 1a

n1

t

2r 1a

n1" #

32

The springback can be obtained from equation (24).

3 RESULTS AND DISCUSSION

To evaluate the two models developed in this study,four materials were selected for comparison. Thematerials used were a mild steel (SCP-1), twoadvanced high strength steels (DP780 and TRIP780),and an aluminium alloy (Al2008). Figure 17 showsthe stress strain relationships for these materials.Table 3 gives the specific tensile properties for thematerials, which are required as input for the models.

Model evaluations were made for sheet thicknessesof 0.7, 1.0, 1.4, 1.7, and 2.0 mm and bending die radiiof 3.175, 6.35, 9.525, 12.7, and 25.4 mm.

Fig. 17 True stresstrue strain curves

Fig. 16 Stress distribution for deformation pattern LC



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To assess the effect of applied strain (stress),approximately ten different values of 1a were used.The range of these applied strain values spannedthe various deformation patterns given in Tables 1and 2.

The values for the parameters a and b in the bend-ing moment model are determined by calculatingtension (T) and are then used in the bendingmoment calculation.

When the applied strain, 1a, is in the elastic range,

the tension (T) in the bending moment model is

calculated as

T tsa tE1a 33

When the applied strain is in the plastic range, thetension (T) in the bending moment model is calcu-lated as

T tsa tK1an 34

Figure 18 shows the predicted springback using theresidual differential strain model (solid lines) and thebending moment model (dotted lines) for two differ-ent combinations of thickness bending radius ofcurvature. With increasing applied strain (1a), thepredicted amount of springback undergoes signifi-cant change. In both models, mild steel (SCP-1) exhi-bits the lowest amount of springback, whereas thealuminium sheet (Al2008) has the largest amount ofspringback. The advanced high strength steels alsoshow significantly higher springback than mild

steel, with the dual phase steel, DP780, exhibitinghigher springback than TRIP780. Both models sortthe materials in the same order with respect tospringback.

For the bending moment model, the springbackgradually decreases with increasing applied strain(1a), whereas the residual differential strain modelshows only a slight decrease until the applied strain(i.e. applied tension) reaches a transition value.

When the applied strain reaches the transition

Table 3 Tensile properties of model materials

Material Elastic modulus (MPa) Yield strength (MPa) Tensile strength (MPa) Strength coefficient K (MPa) n ef

Al 2008 71 000 120 210 490 0.26 13.9SCP-1 2 06 000 160 394 567 0.264 39.0TRIP 780 2 06 000 470 785 1108 0.228 30.0

DP 780 2 06 000 481 843 1200 0.230 19.5

Fig. 18 Comparison of predicted springback between

residual differential strain model (solid lines)

and the bending moment model (dotted

lines) for (a) thickness 1.7 mm, r 6.35 mmand (b) thickness 1.0 mm, r 12.7 mm

Fig. 19 The applied strain transition for the modelbased on residual differential strain



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value, then the springback decreases rapidly andmerges with the model based on the bendingmoment. The transition values for the appliedstrain, as shown in Fig. 19, increase with increasingthickness and decreasing radius of curvature (r).This transition behaviour occurs because theelastic plastic behaviour of sheet metal has threedistinct valid ranges.

Figure 20 compares the variation of springbackwith sheet thickness at different radii of curvatureswithout any applied tension (1a 0). The amountof springback decreases with increasing thickness,and the slopes of the curves calculated from bothmodels show similar trends. Figure 21 compares thevariation of springback with radii of curvatures atdifferent sheet thicknesses without any applied

Fig. 20 Variation of springback with thickness for the

residual differential strain model (solid lines)

and the bending moment model (dotted

lines) for (a) curvature radius 3.175 mm, (b)

curvature radius 9.525 mm, and (c)curvature radius 25.4 mm

Fig. 21 Variation of springback with radius of

curvature for the residual differential strain

model (solid lines) and bending moment

model (dotted lines) for (a) thickness

0.7 mm, (b) thickness 1.4 mm, and (c)thickness 2.0 mm



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tension (1a 0). The amount of springback increaseswith increasing radius of curvature, and the slopesof the curves from both models also show similartrends. According to the evaluation results,the model based on bending moments predicts 25per cent higher springback values than those ofmodels based on residual differential strain for zeroapplied tension.

The residual differentials strain model that hasbeen derived in this study, appears to provide areasonable estimate of springback when comparedto the traditional bending moment model, especially

when the amount of applied tension is sufficientlyhigh. The residual differential strain model producesequations, which are simpler than the bendingmoment model. Experimental verification for bothof these models is still required.

4 SUMMARY

The analysis of the springback of sheet metal duringbending to a radius with applied tensile strainrequires the use of six different deformation pat-terns. These patterns are elastic elastic, plasticelastic, and plasticplastic for the outer and innersurfaces when s0/E5 t/2r and plasticplastic withan elastic core, elasticplastic, and plasticplasticfor the inner and outer surfaces when t/2r5s0/E.Two different analytical models for springback

have been derived. The new model, which is theresidual differential strain model, uses strain differ-ences between the outer and inner surfaces of great-est radius prior to unloading and after elasticrecovery as a measure of springback. The strainson the outer and inner surfaces are calculated forthe loaded condition and after elastic recoveryunder the six different deformation patterns. Thesecond model, which is the traditional bendingmoment model, uses the curvature differencesbetween the loaded and unloaded conditions as ameasure of springback. The moment and the tension

within the strip are calculated for the loaded con-dition. From the moment in the strip, the amountof springback can be determined.

Both models have been compared using four differ-ent materials a low carbon steel, two advanced highstrength steels, and an aluminium alloy. The residualdifferential strain model has an applied transitionstrain, where the springback undergoes a dramaticdecrease. Both models show that springbackdecreases with increased strip thickness and withdecreased radius of curvature. For no applied ten-sion, the bending moment model predicts about25% more springback when compared with the

residual differential strain model. Experimental veri-fication of the models is still required.

ACKNOWLEDGEMENT

This work was partially supported by a grant from theNational Core Research Center (NCRC) programfunded by the Korea Science and Engineering Foun-

dation (KOSEF).

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APPENDIX

Notation

a normalized distance through the thickness ofthe sheet in the moment model

b normalized distance through the thickness ofthe sheet in the moment model

E elastic modulus on loading

Eun effective elastic unloading modulusEu1 effective elastic unloading modulus on theouter surface

Eu2 effective elastic unloading modulus on theinner surface

K strength coefficientm parameter ye/(t/2)n strain hardening exponentSp springback parameterSB springbackt thickness

ye geometrical position of elasticplastic transitionpoint

1a axial strain in combined loading1b bending strain in combined loading1l axial plus bending strain differential

while loaded, 1axial_bending_loading(1axial_tensile_loading

max2 1axial_compressive_loading

max )

1u axial plus bending strain differentialafter unloading, 1axial_bending_unloading(1axial_tensile_unloading

max2 1axial_compressive_unloading

max )1al axial strain while loaded, 1axial_loading1au axial strain after unloading, 1axial_unloading1bl bending strain differential while loaded,1bending_loading(1tensile_loading

max2 1compressive_loading

max )1bu bending strain differential after unloading,

1bending_unloading (1tensile_unloadingmax

2

1compressive_unloadingmax )

1cl largest compressive bending strain(on innersurface) while loaded, 1compressive_loading

max

1cu largest compressive bending strain (on innersurface) after unloading, 1compressive_unloading

max

1tl maximum tensile bending strain (on outer sur-face) while loaded, 1tensile_loading

max

1tu maximum tensile bending strain (on outer sur-face) after unloading, 1tensile_unloading

max

1acl largest axial plus compressive bending strain(on inner surface) while loaded,1axial_compressive_loadingmax

1atl maximum axial plus tensile bending strain (onouter surface) while loaded, 1axial_tensile_loading

max

1acu largest axial plus compressive bendingstrain (on inner surface) after unloading,1axial_compressive_unloadingmax

1atu maximum axial plus tensile bending strain (onouter surface) after unloading,1axial_tensile_unloadingmax

r radius of the curvature.

so yield strengthsun strength of material prior to unloadingsu1 strength of material on the outer surface prior

to unloadingsu2 strength of material on the inner surface prior

to unloading



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Documents

Analytical Prediction of Springback, sheet metal forming