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The International Journal Of Engineering And Science (IJES)
|| Volume || 4 || Issue || 1 || January - 2015 || Pages || 05-08 ||
ISSN (e): 2319 – 1813 ISSN (p): 2319 – 1805
www.theijes.com The IJES Page 5
Study of Damage to ABS Specimens Submitted To Uniaxial
Loading
I.Makadir 1
,M.Barakat2
, M. Elghorba1
, H.Farid3
1.
Laboratoire De Contrôle Et Caractérisation Mécanique Des Matériaux Et Des Structures, École Nationale
Supérieure d’ Électricité Et De Mécanique, Route d'El Jadida. BP 8118 Oasis Casablanca, Maroc
2.
Institut Supérieur des Etudes Maritimes , Route d'El Jadida. BP 8118 Oasis Casablanca, Maroc
3.
Laboratoire De Bioplasturgie Et Nanotechnologie, Université Du Québec Abitibi-Témiscamingue, 445
Boulevard De l’ Université, Rouyn-Noranda, Québec J9X 5E4, Canada
------------------------------------------------ABSTRACT---------------------------------------------------------
Polymers have experienced a remarkable historical development and their use has greatly taxed in our
civilization in a matter of decades gradually overtaking the most ancient materials. These polymer materials
have always distinguished themselves by their simple formatting and inexpensive, their versatility lightness
chemical stability but despite their widespread use both in everyday life and in advanced technologies, these
materials are generally still very misunderstood which requires a thorough knowledge of their chemical,
physical, rheological and mechanical. In this work we focus on the characterization of an ABS plate under uni
axial loading using the unified theory of damage.
KEYWORDS : polymer, breakdown, damage, traction, ABS
-------------------------------------------------------------------------------------------------------------------------------------------
Date of Submission: 15 October 2014 Date of Accepted: 15 January 2015
------------------------------------------------------------------------------------------------------------------------------------------
I. INTRODUCTION
Polymers offer many features that make it appealing, one can distinguish their corrosion features, their
lightness, their low cost, their insulating character their ductility, the many available methods to implement and
shape simultaneously. Or, if one seeks only to their mechanical properties, their behavior is complex and is a
major obstacle [1], as potential users have difficulties to take account in the steps of design and optimization.
However because of the presence of voids in the material, or even damage, cracks can start and propagate to a
size causing the collapse of the structure [2]. To assess the level of damage to a structure subjected to any
solicitation, two models exist: the mechanics of mechanical damage to the rupture [3] and this work is a
contribution to the study of the failure mechanism an ABS plate under urging by the uniaxial tensile test.
II. THEORY
The damage of a material leads to a lowering of the limit of endurance and resistance to static strength
[4]. Gatts's hypothesis [5] to stress above the endurance limit, fatigue damage is a power function of the form:
γD=( γur/ γu)m
with γD=( σD/ σD0) , γur=( σur/ σD0) , γu=( σu/ σD0)
or σD0 is the endurance limit of the virgin material, σD is instantaneous endurance limit of the material (after n
cycles of loading) σur is the instantaneous value of the tensile strength of the material monotonous, σu is the
maximum resistance monotonic tensile virgin material, m is an empirical constant [6]. Bui Quoc model [7]
provides a correlation between the tensile strength and the monotonous cyclic loading, the resistance of a
material to a static effect diminishes if previous efforts undergoes cyclical nature of the application the static
force [8]. We are talking about the reduction of the residual strength of the material [9]. σur (equal to σer for
polymers) is the residual stress of the final damage after n cycles of loading, σu (σe equal to polymers) the
material is virgin material of the ultimate stress, β is the fraction of life and σm = γ / σD0 is the level of loading
(σm average cyclic stress) [10]. for polymers, the ultimate stress σu and the stress at the limit of elasticity σe are
identical [11]. Thus, the parameter m is a parameter material with m = 1 for amorphous [12] polymers. The
formulation proposed by Bui Quoc damage is different from that previously presented by Miner [13]:
D=(1- γD)/ (1- γD
*
)
γD= σD/ σD0 , γD
*
= σm/ σD0
σD : the endurance limit
Study Of Damage To ABS Specimens…
www.theijes.com The IJES Page 6
σD
*
: Critical endurance limit
the damage model resulting fraction is a function of the load and the life of the mechanical properties of the
virgin material [14]:
or γu= σu/ σD0 is a parameter characterizing the virgin material
III. EXPERIMENTAL
To highlight the influence of the notch on the behavior of specimens ABS, a series of tests was carried
out on the characterization of damage on two rectangular sample groups of SBS using the database of ASTM
882 -02 [15] and 766m ASTM D [16]. the first test is smooth on rectangular specimens (without defects) for the
mechanical characterization and the second is on rectangular test specimens with notches of 1mm to 7mm length.
All the experimental tests were carried out under a controlled displacement and the following figure shows the
implementation of the tensile test
Figure 1 Experimental set-up: A test specimen held by the sample holder of the tensile testing machine (left),
and dimensions of the test specimen (right).
IV. RESULTS
It should be noted that the phenomenon of stress concentration is created in notched specimens is
observed and also the notch effect of the reaction which reflects the structure of the force applied depending on
the length of cut.
Figure 2 shows the evolution of the stress versus strain
Figure 2 . Evolution of the stress-strain curves for uniaxial tensile tests on rectangular test specimens according
to ASTM D 882-02 two and ASTM D5766M
Study Of Damage To ABS Specimens…
www.theijes.com The IJES Page 7
In the curves of the figure, we notice a decrease in the resistance threshold of elasticity as the cut
increases in length. After this threshold we observe a short softening stage called "draw hook" that is assigned to
the multiplication of microstructural defects, and a long curing step. These curves also show a remarkable
degradation of the mechanical properties of the material comprising the elastic stress, ultimate tensile stress and
elongation.
Figure 3 : evolution of the maximum stress as a function of the length of notch
Figure 4 : evolution of tensile strength depending on the length of notch
As already mentioned in the curves of the right branch shows the stress-strain response of the sample
elastic, this allows the calculation of the branch Young's modulus. However, with the existence of the cut we'll
talk more stiffness for samples that notched Module young for smooth specimens, stiffness determines the limits
of intervention for elastic structures notched.
Figure 5. Evolution of the damage versus the fraction of life
Study Of Damage To ABS Specimens…
www.theijes.com The IJES Page 8
The figure shows the evolution of damage in notched specimens with a length of cut ranging from 1mm
to 7mm which is a linear variation. At the beginning of the curve we see negligible levels of damage and as the
crack length increases the damage accelerates to a maximum value of 0.98. Or the first installment of the curve
that represents the initiation zone characterizes the highest mechanical properties of the material until the last
break point represents degradation. This approach is proposed by analogy with the cumulative damage theory
proposed by Gatts [17] Bui Quoc- by [9] to show the evolution of damage in a structure ABS.
V. CONCLUSION
The aim of our study was to assess the level of damage ABS thermoplastic plates subjected to uniaxial
stress. We have found that the tensile test is the most effective approach to approximate the actual deformation
of the structure during the loading technique. This Require to agree on the use of the unified theory of damage in
the interest of present closer to the actual state of damage model. With the aim to provide a formulation of the
damage depends only loading conditions of the mechanical properties of virgin material, we looked at the model
Bui Quoc, and the results showed the use of this approach is therefore to describe strictly the state of matter.
This preliminary work is a necessary step to achieve our goals completely and develop other tools to simulate the
microstructural degradation phenomenon structures ABS.
REFERENCES
[1] Sanchez-Santana U., Comportement dynamique des matériaux et structures après sollicitation en fatigue. Thèse de doctorat,
Université des sciences et technologies de Lille, 2007.
[2] Criens R.M. and Moslé H.G., Faillure of plastics, edited by W. Brostow and R.D. Corneliunssen Hauser, 1986.
[3] Brostow W., Kubàt J. and Kubàt M., Physical properties of polymers handbook, Chapter 23: Mechanical properties, American
Institute of physics, James E. Mark editor, 1996.
[4] Lemaitre J. andChaboche J.L., Aspect phénoménologique de la rupture par endommagement, journal de la mécanique appliquée,
Vol 2, 1978.
[5] Shia-Chung C., Rheologicalbehavior of PS polymer melt under ultra-high speed injection molding, Polymer Testing Journal,
Volume 31, Issue 7, October 2012.
[6] Erchiqui1 F., Ozdemir Z., Souli M., Ezzaidi H., Dituba-Ngoma G., Neural networks approach for characterization of viscoelastic
polymers, volume 89, Issue 5, October 2011.
[7] Figueredo R., Cherouat A., Une nouvelle approche dans la prise en compte de la déformation permanente et volumique induite
par l’ endommagement dans la mise en forme des structures caoutchoutiques, 19 ème Congrès Français de Mécanique, Marseille
2009.
[8] Davis J.R., Tensile testing second edition, ASM International, The material information society 2004.
[9] Bui-Quoc T., Dubuc J., Bazergui A., Biron A., Cumulative fatigue damage under stress-controlled conditions, Journal of Basic
Engineering, Transactions of the ASME, 1971.
[10] Miner M., Cumulative damage in fatigue, Journal of Applied Mechanics, Volume 12, 1945.
[11] Jardin A., Leblond J.B., Berghezan D., Par-delà la loi de Miner pour la modélisation de la fatigue des élastomères : théorie et
expérimentation, 19 ème Congrès Français de Mécanique, Marseille 2009.
[12] Miller K.J., Zachariah K.P, Cumulative damage fatigue crack initiation and state I propagation, Journal of Strain Analysis, 1977.
[13] Lemaitre J, Chaboche J.L, Mechanics of Solid Materials, Cambridge University Press, Cambridge, UK, 1990.
[14] D 882-02 ASTM Standard test method for tensile properties of thin plastic sheeting.
[15] D5766M ASTM Standard test method for open hole tensile strength of polymer matrix composite laminates.
[16] E606 / E606M - 12 ASTM Standard Test Method for Strain-Controlled Fatigue Testing.
[17] Gatts R., Application of cumulative damage concept to fatigue, ASTM Transactions, Journal of basic engineering, Volume 83,
1961.
[18] LemaignanC., La Rupture des matériaux, EDP Sciences 2003.
[19] Boresi A.P., Sidebottom O.M., Advanced mechanics of materials 4th edition, John Wiley and sons 1985.
[20] Lemaitre J, Chaboche J.L, Mécanique des matériaux solides 3ème édition, Edition Dunod 2009.

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Study of Damage to ABS Specimens Submitted To Uniaxial Loading

  • 1. The International Journal Of Engineering And Science (IJES) || Volume || 4 || Issue || 1 || January - 2015 || Pages || 05-08 || ISSN (e): 2319 – 1813 ISSN (p): 2319 – 1805 www.theijes.com The IJES Page 5 Study of Damage to ABS Specimens Submitted To Uniaxial Loading I.Makadir 1 ,M.Barakat2 , M. Elghorba1 , H.Farid3 1. Laboratoire De Contrôle Et Caractérisation Mécanique Des Matériaux Et Des Structures, École Nationale Supérieure d’ Électricité Et De Mécanique, Route d'El Jadida. BP 8118 Oasis Casablanca, Maroc 2. Institut Supérieur des Etudes Maritimes , Route d'El Jadida. BP 8118 Oasis Casablanca, Maroc 3. Laboratoire De Bioplasturgie Et Nanotechnologie, Université Du Québec Abitibi-Témiscamingue, 445 Boulevard De l’ Université, Rouyn-Noranda, Québec J9X 5E4, Canada ------------------------------------------------ABSTRACT--------------------------------------------------------- Polymers have experienced a remarkable historical development and their use has greatly taxed in our civilization in a matter of decades gradually overtaking the most ancient materials. These polymer materials have always distinguished themselves by their simple formatting and inexpensive, their versatility lightness chemical stability but despite their widespread use both in everyday life and in advanced technologies, these materials are generally still very misunderstood which requires a thorough knowledge of their chemical, physical, rheological and mechanical. In this work we focus on the characterization of an ABS plate under uni axial loading using the unified theory of damage. KEYWORDS : polymer, breakdown, damage, traction, ABS ------------------------------------------------------------------------------------------------------------------------------------------- Date of Submission: 15 October 2014 Date of Accepted: 15 January 2015 ------------------------------------------------------------------------------------------------------------------------------------------ I. INTRODUCTION Polymers offer many features that make it appealing, one can distinguish their corrosion features, their lightness, their low cost, their insulating character their ductility, the many available methods to implement and shape simultaneously. Or, if one seeks only to their mechanical properties, their behavior is complex and is a major obstacle [1], as potential users have difficulties to take account in the steps of design and optimization. However because of the presence of voids in the material, or even damage, cracks can start and propagate to a size causing the collapse of the structure [2]. To assess the level of damage to a structure subjected to any solicitation, two models exist: the mechanics of mechanical damage to the rupture [3] and this work is a contribution to the study of the failure mechanism an ABS plate under urging by the uniaxial tensile test. II. THEORY The damage of a material leads to a lowering of the limit of endurance and resistance to static strength [4]. Gatts's hypothesis [5] to stress above the endurance limit, fatigue damage is a power function of the form: γD=( γur/ γu)m with γD=( σD/ σD0) , γur=( σur/ σD0) , γu=( σu/ σD0) or σD0 is the endurance limit of the virgin material, σD is instantaneous endurance limit of the material (after n cycles of loading) σur is the instantaneous value of the tensile strength of the material monotonous, σu is the maximum resistance monotonic tensile virgin material, m is an empirical constant [6]. Bui Quoc model [7] provides a correlation between the tensile strength and the monotonous cyclic loading, the resistance of a material to a static effect diminishes if previous efforts undergoes cyclical nature of the application the static force [8]. We are talking about the reduction of the residual strength of the material [9]. σur (equal to σer for polymers) is the residual stress of the final damage after n cycles of loading, σu (σe equal to polymers) the material is virgin material of the ultimate stress, β is the fraction of life and σm = γ / σD0 is the level of loading (σm average cyclic stress) [10]. for polymers, the ultimate stress σu and the stress at the limit of elasticity σe are identical [11]. Thus, the parameter m is a parameter material with m = 1 for amorphous [12] polymers. The formulation proposed by Bui Quoc damage is different from that previously presented by Miner [13]: D=(1- γD)/ (1- γD * ) γD= σD/ σD0 , γD * = σm/ σD0 σD : the endurance limit
  • 2. Study Of Damage To ABS Specimens… www.theijes.com The IJES Page 6 σD * : Critical endurance limit the damage model resulting fraction is a function of the load and the life of the mechanical properties of the virgin material [14]: or γu= σu/ σD0 is a parameter characterizing the virgin material III. EXPERIMENTAL To highlight the influence of the notch on the behavior of specimens ABS, a series of tests was carried out on the characterization of damage on two rectangular sample groups of SBS using the database of ASTM 882 -02 [15] and 766m ASTM D [16]. the first test is smooth on rectangular specimens (without defects) for the mechanical characterization and the second is on rectangular test specimens with notches of 1mm to 7mm length. All the experimental tests were carried out under a controlled displacement and the following figure shows the implementation of the tensile test Figure 1 Experimental set-up: A test specimen held by the sample holder of the tensile testing machine (left), and dimensions of the test specimen (right). IV. RESULTS It should be noted that the phenomenon of stress concentration is created in notched specimens is observed and also the notch effect of the reaction which reflects the structure of the force applied depending on the length of cut. Figure 2 shows the evolution of the stress versus strain Figure 2 . Evolution of the stress-strain curves for uniaxial tensile tests on rectangular test specimens according to ASTM D 882-02 two and ASTM D5766M
  • 3. Study Of Damage To ABS Specimens… www.theijes.com The IJES Page 7 In the curves of the figure, we notice a decrease in the resistance threshold of elasticity as the cut increases in length. After this threshold we observe a short softening stage called "draw hook" that is assigned to the multiplication of microstructural defects, and a long curing step. These curves also show a remarkable degradation of the mechanical properties of the material comprising the elastic stress, ultimate tensile stress and elongation. Figure 3 : evolution of the maximum stress as a function of the length of notch Figure 4 : evolution of tensile strength depending on the length of notch As already mentioned in the curves of the right branch shows the stress-strain response of the sample elastic, this allows the calculation of the branch Young's modulus. However, with the existence of the cut we'll talk more stiffness for samples that notched Module young for smooth specimens, stiffness determines the limits of intervention for elastic structures notched. Figure 5. Evolution of the damage versus the fraction of life
  • 4. Study Of Damage To ABS Specimens… www.theijes.com The IJES Page 8 The figure shows the evolution of damage in notched specimens with a length of cut ranging from 1mm to 7mm which is a linear variation. At the beginning of the curve we see negligible levels of damage and as the crack length increases the damage accelerates to a maximum value of 0.98. Or the first installment of the curve that represents the initiation zone characterizes the highest mechanical properties of the material until the last break point represents degradation. This approach is proposed by analogy with the cumulative damage theory proposed by Gatts [17] Bui Quoc- by [9] to show the evolution of damage in a structure ABS. V. CONCLUSION The aim of our study was to assess the level of damage ABS thermoplastic plates subjected to uniaxial stress. We have found that the tensile test is the most effective approach to approximate the actual deformation of the structure during the loading technique. This Require to agree on the use of the unified theory of damage in the interest of present closer to the actual state of damage model. With the aim to provide a formulation of the damage depends only loading conditions of the mechanical properties of virgin material, we looked at the model Bui Quoc, and the results showed the use of this approach is therefore to describe strictly the state of matter. This preliminary work is a necessary step to achieve our goals completely and develop other tools to simulate the microstructural degradation phenomenon structures ABS. REFERENCES [1] Sanchez-Santana U., Comportement dynamique des matériaux et structures après sollicitation en fatigue. Thèse de doctorat, Université des sciences et technologies de Lille, 2007. [2] Criens R.M. and Moslé H.G., Faillure of plastics, edited by W. Brostow and R.D. Corneliunssen Hauser, 1986. [3] Brostow W., Kubàt J. and Kubàt M., Physical properties of polymers handbook, Chapter 23: Mechanical properties, American Institute of physics, James E. Mark editor, 1996. [4] Lemaitre J. andChaboche J.L., Aspect phénoménologique de la rupture par endommagement, journal de la mécanique appliquée, Vol 2, 1978. [5] Shia-Chung C., Rheologicalbehavior of PS polymer melt under ultra-high speed injection molding, Polymer Testing Journal, Volume 31, Issue 7, October 2012. [6] Erchiqui1 F., Ozdemir Z., Souli M., Ezzaidi H., Dituba-Ngoma G., Neural networks approach for characterization of viscoelastic polymers, volume 89, Issue 5, October 2011. [7] Figueredo R., Cherouat A., Une nouvelle approche dans la prise en compte de la déformation permanente et volumique induite par l’ endommagement dans la mise en forme des structures caoutchoutiques, 19 ème Congrès Français de Mécanique, Marseille 2009. [8] Davis J.R., Tensile testing second edition, ASM International, The material information society 2004. [9] Bui-Quoc T., Dubuc J., Bazergui A., Biron A., Cumulative fatigue damage under stress-controlled conditions, Journal of Basic Engineering, Transactions of the ASME, 1971. [10] Miner M., Cumulative damage in fatigue, Journal of Applied Mechanics, Volume 12, 1945. [11] Jardin A., Leblond J.B., Berghezan D., Par-delà la loi de Miner pour la modélisation de la fatigue des élastomères : théorie et expérimentation, 19 ème Congrès Français de Mécanique, Marseille 2009. [12] Miller K.J., Zachariah K.P, Cumulative damage fatigue crack initiation and state I propagation, Journal of Strain Analysis, 1977. [13] Lemaitre J, Chaboche J.L, Mechanics of Solid Materials, Cambridge University Press, Cambridge, UK, 1990. [14] D 882-02 ASTM Standard test method for tensile properties of thin plastic sheeting. [15] D5766M ASTM Standard test method for open hole tensile strength of polymer matrix composite laminates. [16] E606 / E606M - 12 ASTM Standard Test Method for Strain-Controlled Fatigue Testing. [17] Gatts R., Application of cumulative damage concept to fatigue, ASTM Transactions, Journal of basic engineering, Volume 83, 1961. [18] LemaignanC., La Rupture des matériaux, EDP Sciences 2003. [19] Boresi A.P., Sidebottom O.M., Advanced mechanics of materials 4th edition, John Wiley and sons 1985. [20] Lemaitre J, Chaboche J.L, Mécanique des matériaux solides 3ème édition, Edition Dunod 2009.