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A mathematical relation between volume strain, elongational

strain and stress in homogeneous deformation

Citation for published version (APA):

Heikens, D., Sjoerdsma, S. D., & Coumans, W. J. (1981). A mathematical relation between volume strain, elongational strain and stress in homogeneous deformation. Journal of Materials Science, 16(2), 429-432. https://doi.org/10.1007/BF00738633

DOI:

10.1007/BF00738633

Document status and date: Published: 01/01/1981

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J O U R N A L O F M A T E R I A L S S C I E N C E 1 6 ( 1 9 8 1 ) 4 2 9 - 4 3 2

A mathematical relation between volume

strain, elongational strain and stress in

homogeneous deformation

D E R K H E I K E N S , S. D I R K S J O E R D S M A , W. J A N C O U M A N S

Eindhoven University of Technology, Eindhoven, The Netherlands

A model is presented for the volume strain of a two-phase blend which elongates homo- geneously in a tensile test apparatus. In the case when only elastic deformation and crazing take place the volume strain against elongation curve can be constructed and cal- culated from the data of the stress-strain curve alone. When, as well as crazing and elastic deformation, shearing takes place, the data of the stress against elongation curve and the volume strain against elongation curve can be used to calculate the separate contributions of the three deformation mechanisms at any elongation. In principle, the model can be also used for any homogeneous system which deforms without necking and where one or more deformation mechanism is present.

1. Introduction

In order to study mechanical deformation of two- phase polystyrene (PS)-low-density polyethylene (PE) blends and of high impact polystyrene a dilatometer was developed to determine volume strain during tensile deformation [ 1 - 3 ] . The results prompted the development of a simple model that describes the volume strain as a func- tion of stress and strain for constant strain-rate experiments. Assuming the additivity of volume strain and elongational strain caused by elasticity, crazing and shearing, as was done for creep tests by Bucknall [ 4 - 6 ] , it is possible to write

AVIVo

= ( A V e l + A V s h + AVe~)IVo

= (AV/Vo)el + (AV/Vo)sh + (AV/Vo)e~,

( 1 ) where A V is the change in volume strain, Vo is the zero-strain volume, and AVel , AVsh and AVe~ are the change in components of volume strain caused by elasticity, shearing and crazing.

e = Al/lo = (a/el + A/sh + Aler)/lo

= e e l + e s h + e e r , (2) where e is the elongation strain, Al is the change in length, lo is the zero-strain length, A/el , A/sh 0022-2461/81/020429-04502.40/0

and Alc~ are the changes in length due to elasticity, shearing and crazing and eel, esh and ee~ are the contributions to the elongation strain caused by elasticity, shearing and crazing.

From the definition of Poisson's ratio, uel, (AV/Vo)el = (1 - - 2Vel)eel, ( 3 ) while

O

eel = ~ , (4)

where a is the stress and E is Young's modulus. The contribution of crazing to the volume strain is given by

(AV/Vo)e~ = ec~, ( 5 )

while

(AV/Vo)sh = 0. (6)

Thus,

AV/Vo = eel(1 -- 2Vel) + eer (7) o r

AV/Vo

= e e l ( 1 - - 2 P e l ) -1- e - - e s h - - eel , ( g ) where eel may be set equal to o/E for all values of esh and eer when the amount of material subjected

to elastic deformation is constant.

In the case of the PS-(low-density)PE blends mentioned above, the total elongation-to-break is about 10 per cent, of which 1 to 2 per cent is

(3)

elastic. In case of crazing only, the void content is then ultimately about 8 per cent. Assuming that a n approximately equal fraction of the sample material is transformed into craze-filling material, the amount of matrix available to deform elast- icaUy will always be higher than 92 per cent. This means that the elongation, eel, should be corrected by a factor, A, where 0.92 < A < 1. When the matrix also deforms by shear the same factors must be considered. As a first approximation, however, Equation 8 will be correct.

2. Crazing and elastic d e f o r m a t i o n o n l y

In many high-impact polystyrenes shearing is negligible and Equation 8 reduces to

E o (9)

AV/Vo = (1--2Ve]) + e E" Again, the first term represents the elastic contri- bution to the volume strain and the following two terms the contribution of crazing. Rearrangement gives

(5

AVlVo

= e - 2Ve~-~.

(10)

Equation 10 can be used to calculate the volume strain against elongational strain curve from a stress-strain curve. The stress, (5, is approximated by the engineering stress and the Young'smodulus, E, is taken as the initial slope of the stress-strain curve. Poisson's ratio is either known or can be calculated from the initial slope of the volume strain against elongational strain curve. For any point, (e, (5), of a given stress-strain curve (see

((;I 9 1 E)

]

llAVIVoIcr /

~l-~uet;~

~ - T u l : I ^ I/1t1__ ] I 9 s ~r s 9

Figure 1 Construction of a volume strain curve from a known stress-strain curve.

I

/ E g

A~IVo)c r

~vlvo) ~

Figure 2 Construction of a volume strain curve from a known stress-strain curve.

Fig. 1), eel can be found by means of the pro- portional relation (5 = Eccl.

Since a series model for strains is assumed, %x is the difference between e and %1. Now the contribution of the elastic deformation to the total volume strain for the point (e, (5) can be found from the relation (AV/Vo) = (1--2Pel) eel. The contribution of crazing to the total volume strain, (AV/Vo)~=ec~. In Fig. 1 (for one point) and in Fig. 2 (for all points) these contributions are calculated from a given stress-- strain curve.

The slope of the volume strain against elong- ation curve is given by Equation 11

d(AV/Vo) 212el do

- 1 ( 1 1 )

de E de"

Since, after yielding, d(5/de is negative, d(A V/V o)~ de must be greater than 1. It becomes clear that a high value of gradient (> 1) results from the stress drop after the yield-point due to a rate of void formation which is high compared to the rate of elongation. At the yield-point and at high elongation values, where do/de = 0, the slopes of the volume strain curve are equal to one. It is evident that void formation by crazing is initiated before the stress maximum at a point (el, oi) (Fig. 2).

The general features predicted by the model are confirmed by experimental curves of P S - (low-density)PE blends. In Figs 3 and 4 the experi- mental results are presented for a commercial high-impact polystyrene and for a P S - P E blend 430

(4)

O.lO o.o8-

"~ 0.06

-

i:::

?o.o4- 0 , 0 2 -

O-

~ed /

lume

I

i ,i

"

O:Z

1000 -800 -600~ -400 i

-200

-0

i

,i

0:4 06 ~" Al(cm)

Figure 3 Experimental curves of load against elongation

and of volume strain against elongational strain of high- impact polystyrene (Dew Chemical Co.). The change in sensitivity of volume strain Al was about Al= 0.4. Volume strain calculated using Equation 9 from the stress-strain curve is represented by dots. The experi- mentally determined results are represented by the full lines. Maximum slope of volume strain, d ( A V / V o)/de =

1.06.

[ 1]. The full curves are experimentally determined whereas the dots have ~ V and e as co-ordinates and are calculated from Equation 9. As the true stress deviates by less than one per cent from the

0.12 -

/ - 1 2

0.10-

0.08- 8 z ---

0.06-

X

t

0.04-

4 T

0.02 -

0-

i ! ,I il ,I 0

0

0.2

0.4 ,L AI (cm)

Figure 4 Experimental curves, as in Fig. 3, for a PS-

(low-density)PE blend (92.5 vol% PS-7.5 vol% PE. Dots calculated using Equation 9. Maximum slope of volume strain, d (4 V / V o )/de = I. 14.

engineering stress, a value o f the engineering stress was used instead o f a true stress value. E and were taken from the initial slopes o f the stress and volume strain curve. The agreement between the m o d e l and experimental results is very good. The m a x i m u m slopes of the volume strain curves for these cases are greater than one and are given in captions o f Figs 3 and 4.

3. The deformation mechanisms present

For ABS, and for some special PS-(low-density)PE

blends containing certain block co-polymers, b o t h crazing and shearing are found [1] as deformation mechanisms. Rearrangement o f Equation 8 gives

esh = ( 1 - - 2 % 1 ) ~ - + - - - - A V / V o . (12) The sum of the first two terms o f Equation 12 represents the volume change o f a h y p o t h e t i c a l material with the same s t r e s s - s t r a i n curve in which no shearing but only elastic deformation and crazing takes place during elongation. Thus %5 can be calculated by combining the data from the s t r e s s - s t r a i n curve and the volume strain curve. Also, eex can be found from Equation 7 by subtracting the elastic c o n t r i b u t i o n to the volume strain, (1 - - 2%1 ) ~ / E from the experimental volume strain giving

O

ecr = A x V / V o - - (1 - - 2%1 ) ~-. (13)

These results are shown in Fig. 5 using h y p o t h e t i c a l

a (AV/V O) no

shear

= /

E; , ~ ( 1 - 2 l ; e I )

o'/E +E -~

/

I (A V/re)el = (I-2%1) olE

- - E

Figure 5 Estimation of the contribution of shearing,

crazing and elastic deformation to the total elougation from hypothetical stress and volume strain-elongation curves.

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stress-strain and volume strain-elongational strain curves. Of special interest are the parts of a stress- elongation curve where

de/de = 0. (14)

Differentiating Equations 12 and 13 yields

d(AxV/Vo) 1 desh _ de= (15)

de de de

This shows that for cases where de/de ~ 0, for instance at the yield-point or in some cases at large elongations, the slope of the volume strain curve is a direct measure of the incremental contri- butions desh/de and deer/de at the corresponding elongation. This analysis was applied in [1 ].

For creep experiments, where de/de is prac- tically zero, the slope at any point on the volume strain against elongational strain curve is a measure of the strain contributions of the two mechanisms. This principle has been used by Bucknall for a number of materials that deform by crazing [7].

The model developed for heterogeneous systems should also be applicable to homogeneous mater- ials deforming without necking, provided that

mechanisms like sheafing and crazing do not greatly diminish the volume of the material that is deforming elastically. However, as the volume effect on the elastic deformation is usually rather small in the region of crazing, deviations from the model will still be small, and the model will there- fore still be applicable.

References

1. W. JAN COUMANS, DERK HEIKENS and S. DIRK

SJOERDSMA, Polymer 21 (1980) 103.

2. W. JAN COUMANS and DERK HEIKENS, Polymer

21 (1980) 957.

3. W. JAN COUMANS, DERK HEIKENS and S. DIRK

SJOERDSMA, International Union of Pure and Applied Chemistry 26th International Symposium on Macromolecules, Mainz, September, 1979, Vol. III, edited by I. Liiderwald and R. Weis, p. 1389.

4. C.B. BUCKNALL and D. CLAYTON, Nature 231

(1971) 107.

5. Idem, J. Mater. ScL 7 (1972) 202.

6. C. B. BUCKNALL, D. CLAYTON andW. E. KEAST,

J. Mater. ScL 7 (1972) 1443.

7. C.B. BUCKNALL, "Toughened Plastics" (Applied

Science Publishers, London, 1977).

Received 6 March 1980 and accepted 10 July 1980.

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