A Simscape Based Mesostructural Model of Skin...

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A Simscape Based Mesostructural Model of Skin Mechanics Andrei Pissarenko 1 , Wen Yang 2 , Haocheng Quan 3 , Katherine A. Brown 5,7 , Alun Williams 4 , William G. Proud 5,6 , Marc A. Meyers 1,3 Skin is the outermost layer of our bodies, as well as the largest organ. It acts as a first protective barrier against external agents such as heat, light, infection, and injury. Skin carries a vast network of nerves, glands and vessels that enable sensing of heat, touch, pressure and pain, and is also a crucial interface that regulates our body temperature and stores water and lipids in order to maintain a healthy metabolism [1]. In order to fulfill such a broad range of functions throughout an individual’s life, skin must be able to withstand and recover from tremendous deformations as well as mitigate tear propagation that can occur during growth, movement, and potential injuries that affect its integrity. As a result, characterizing the viscoelastic behavior of skin and understanding the underlying mechanisms of deformation at different levels of scale is essential in a large spectrum of applications such as surgery, cosmetics, forensics, biomimicry and engineering of protective gear or artificial grafts, for example. Although a fair amount of research has focused on skin’s non-linear elastic and viscoelastic properties at various structural levels [2,3], proposed models often neglect said levels of complexity and lean towards a phenomenological approach rather than a micromechanical model. Other models accounting for fiber dispersion in skin are generally limited by their complexity and inadaptability, The present study proposes a new framework to describe skin mechanics, using a Simscape physical component model [4] which enables rapid parameter identification and offers malleability via its block-based structure. Interactions between constitutive elements are simulated using a microstructural Finite Element Model. Experimental Methods Two 9 weeks old piglets were sacrificed and their skin was surgically excised. The fat layer was removed with a scalpel and ASTM D412 Type B [5] samples were obtained using a cutting die. Cuts from the back and the belly were performed in two distinct directions: along the direction of the spine ( longitudinal cut), and perpendicular to it (transverse cut). Skin was tested fresh. Setup for tensile tensing Modeling Interactions Between Components 0 5 10 15 20 25 30 35 1.00E-04 1.00E-03 1.00E-02 1.00E-01 1.00E+00 Engineering Stress (MPa) Strain Rate (s -1 ) Failure Stress vs. Strain Rate 0 2 4 6 8 10 12 14 16 18 20 0 0.2 0.4 0.6 Engineering Stress (MPa) Engineering Strain Strain Rate Sensitivity of Pig Skin 0.0001 mm/mm/s 0.001 mm/mm/s 0.01 mm/mm/s 0.1 mm/mm/s 1 mm/mm/s DIC analysis of a pig skin sample in tension. 2D mapping of the vertical displacement Samples were speckled and tensile tests were recorded using a Phantom v120 High-Speed Camera Acknowledgements Support from a Multi-University Initiative through the Air Force Office of Scientific Research (AFOSR- FA9550-15-1-0009) to the University of California Riverside with a subcontract to the University of California San Diego. References [1] G. J. Tortora, B. Derrickson, Principles of Anatomy and Physiology, John Wiley and Sons, Inc., 2009. [2] W. Li, Biomed. Eng. Lett. 5 (2015) 241250. [3] G. Limbert, Proc. R. Soc. A Math. Phys. Eng. Sci. 473 (2017) [4] https://www.mathworks.com/products/simscape ; [5] https://www.astm.org/Standards/ D412; [6] http://ncorr. com [7] J.W.Y. Jor, M.P. Nash, P.M.F. Nielsen, P.J. Hunter, Biomech. Model. Mechanobiol. 10 (2011) 767778. [8] R. Meijer, L.F. a. Douven, C.W.J. Oomens, Comput. Methods Biomech. Biomed. Engin. 2 (1999) 1327 [9] W. Yang, V.R. Sherman, B. Gludovatz, E. Schaible, P. Stewart, R.O. Ritchie, M.A. Meyers, Nat. Commun. 6 (2015) 6649. [10] S.E. Szczesny, D.M. Elliott, Acta Biomater. 10 (2014) 25822590 [11] W. Li, X.Y. Luo, Ann. Biomed. Eng. 44 (2016) 31093122. [12] M.B. Rubin, S.R. Bodner, Int. J. Solids Struct. 39 (2002) 50815099 Conclusions and Future Work 0.55 0.6 0.65 0.7 0.75 0.8 0.85 0.9 0.95 1 0 0.2 0.4 Normalized Stress Time (min) Stress Relaxation at increasing strains 15.4% 24.6% 28.8% 33.8% 1 Department of Mechanical and Aerospace Engineering, University of California, San Diego, CA, USA. 2 Materials Sciences Division, Lawrence Berkeley National Laboratory, USA. 3 Department of Material Science and Engineering, University of California, San Diego, CA, USA. 4 Department of Veterinary Medicine, University of Cambridge, Cambridge, UK. 5 The Royal British Legion Centre for Blast Injury Studies, Imperial College London, London, UK. 6 Institute of Shock Physics, Imperial College London, London, UK Department of Chemistry, 7 The University of Texas at Austin, Austin, Texas, United States. In the block model, elements can be easily rearranged, modified. Resolution is very fast with the Parameter Estimation Module Can be applied to a broad range of loading conditions - Strain Rate Sensitivity - Stress Relaxation & Creep - Cyclic Loading Limited to uniaxial tests Necessity to better understand the structural arrangement in the dermis TEM, SEM, Confocal Imaging… Some more in-depth energy dissipative processes can be added -Friction -Shear-Lag [10] -Damage evolution [11,12] FEA, Molecular Dynamics. (resolution:512x512; frame rates: 10fps, 20fps, 80fps). The Matlab software Ncorr 2.1 [6] was used to perform DIC and estimate sample slipping. Experimental Results 0 2 4 6 8 10 0 0.1 0.2 0.3 0.4 Engineering Stress (MPa) Engineering Strain Loading/Unloading Tests 16% 35% 40% Scanning Electron Micrograph of a Collagen Fiber in the dermis of pig skin The principal load-bearing component of skin is the dermis, composed of collagen (~30% v.f.) [7,8], elastin (~2% v.f.) [7,8] and a soft viscoelastic matrix. Collagen fibrils form bundles, which are initially crimped. We describe the waviness of the fibers using a semi- circular model [9], with: - 0 : initial radius - 0 : crimp angle - : fiber thickness The deformation of such a fiber is expressed by: =න 0 () Where is the apparent Young’s Modulus along the axis of tension, defined by the structural parameters listed above. Linear Elastic Neo-Hookean S-shaped Model Tensile Test of Pig Skin (Transverse) at 10 -2 s -1 = 100 ⋅ Influence of the strain rate = 136 0 = 8.9 0 = 54° = 4 = 17° = 1 = 58 = 7.46 6 = 4.65 5 Mesostructural Simscape Model Periodic Representative Volume Element in tension (Abaqus Finite Element Model) Crimped Collagen Fibers spaced apart with a given distance Embedded in a hyperelastic matrix Averaged Stress vs. Strain in the RVE for different values of μ (E=200GPa) TEM,SEM, SAXSFEA Block Model Structural Arrangement Experiments Constitutive and Structural Parameters of Skin Interactions

Transcript of A Simscape Based Mesostructural Model of Skin...

  • A Simscape Based Mesostructural Model of Skin MechanicsAndrei Pissarenko1, Wen Yang2, Haocheng Quan3, Katherine A. Brown5,7, Alun Williams4, William G. Proud5,6, Marc A. Meyers1,3

    Skin is the outermost layer of our bodies, as well as the largest organ. It acts as a first protective barrier against external agents such as heat, light, infection, and injury. Skin carries a vast network of nerves, glands and vessels that enable sensing of heat, touch, pressure and pain, and is also a crucial

    interface that regulates our body temperature and stores water and lipids in order to maintain a healthy metabolism [1].

    In order to fulfill such a broad range of functions throughout an individual’s life, skin must be able to withstand and recover from tremendous deformations as well as mitigate tear propagation that can occur during growth, movement, and potential injuries that affect its integrity.

    As a result, characterizing the viscoelastic behavior of skin and understanding the underlying mechanisms of deformation at different levels of scale is essential in a large spectrum of applications such as surgery, cosmetics, forensics, biomimicry and engineering of protective gear or artificial

    grafts, for example.

    Although a fair amount of research has focused on skin’s non-linear elastic and viscoelastic properties at various structural levels [2,3], proposed models often neglect said levels of complexity and lean towards a phenomenological approach rather than a micromechanical model. Other models accounting

    for fiber dispersion in skin are generally limited by their complexity and inadaptability, The present study proposes a new framework to describe skin mechanics, using a Simscape physical component model [4] which enables rapid parameter identification and offers malleability via its block-based

    structure. Interactions between constitutive elements are simulated using a microstructural Finite Element Model.

    Experimental MethodsTwo 9 weeks old piglets were sacrificed and their skin was surgically excised. The fat layer was

    removed with a scalpel and ASTM D412 Type B [5] samples were obtained using a cutting die.

    Cuts from the back and the belly were performed in two distinct directions: along the direction of

    the spine ( longitudinal cut), and perpendicular to it (transverse cut). Skin was tested fresh.

    Setup for tensile tensing

    Modeling Interactions Between Components

    0

    5

    10

    15

    20

    25

    30

    35

    1.00E-04 1.00E-03 1.00E-02 1.00E-01 1.00E+00

    Engin

    eering S

    tre

    ss

    (MP

    a)

    Strain Rate (s-1)

    Failure Stress vs. Strain Rate

    0

    2

    4

    6

    8

    10

    12

    14

    16

    18

    20

    0 0.2 0.4 0.6

    Engin

    eerin

    g S

    tress (

    MP

    a)

    Engineering Strain

    Strain Rate Sensitivity of Pig Skin

    0.0001 mm/mm/s

    0.001 mm/mm/s

    0.01 mm/mm/s

    0.1 mm/mm/s

    1 mm/mm/s

    DIC analysis of a pig skin sample in tension.

    2D mapping of the vertical displacement

    Samples were speckled and

    tensile tests were recorded

    using a Phantom v120

    High-Speed Camera

    AcknowledgementsSupport from a Multi-University Initiative through the Air Force Office of Scientific Research (AFOSR-

    FA9550-15-1-0009) to the University of California Riverside with a subcontract to the University of

    California San Diego.

    References[1] G. J. Tortora, B. Derrickson, Principles of Anatomy and Physiology, John Wiley and Sons, Inc., 2009.[2] W. Li, Biomed. Eng. Lett. 5 (2015) 241–250.

    [3] G. Limbert, Proc. R. Soc. A Math. Phys. Eng. Sci. 473 (2017)

    [4] https://www.mathworks.com/products/simscape ; [5] https://www.astm.org/Standards/D412; [6] http://ncorr.com

    [7] J.W.Y. Jor, M.P. Nash, P.M.F. Nielsen, P.J. Hunter, Biomech. Model. Mechanobiol. 10 (2011) 767–778.

    [8] R. Meijer, L.F. a. Douven, C.W.J. Oomens, Comput. Methods Biomech. Biomed. Engin. 2 (1999) 13–27

    [9] W. Yang, V.R. Sherman, B. Gludovatz, E. Schaible, P. Stewart, R.O. Ritchie, M.A. Meyers, Nat. Commun. 6 (2015) 6649.

    [10] S.E. Szczesny, D.M. Elliott, Acta Biomater. 10 (2014) 2582–2590

    [11] W. Li, X.Y. Luo, Ann. Biomed. Eng. 44 (2016) 3109–3122.

    [12] M.B. Rubin, S.R. Bodner, Int. J. Solids Struct. 39 (2002) 5081–5099

    Conclusions and Future Work

    0.55

    0.6

    0.65

    0.7

    0.75

    0.8

    0.85

    0.9

    0.95

    1

    0 0.2 0.4

    Norm

    aliz

    ed S

    tress

    Time (min)

    Stress Relaxation at increasing strains

    15.4%

    24.6%

    28.8%

    33.8%

    1Department of Mechanical and Aerospace Engineering, University of California, San Diego, CA, USA. 2Materials Sciences Division, Lawrence Berkeley National Laboratory, USA. 3Department of Material Science and Engineering,

    University of California, San Diego, CA, USA. 4Department of Veterinary Medicine, University of Cambridge, Cambridge, UK. 5The Royal British Legion Centre for Blast Injury Studies, Imperial College London, London, UK. 6Institute of

    Shock Physics, Imperial College London, London, UK Department of Chemistry, 7The University of Texas at Austin, Austin, Texas, United States.

    • In the block model, elements can be

    easily rearranged, modified.

    • Resolution is very fast with the

    Parameter Estimation Module

    • Can be applied to a broad range of

    loading conditions

    - Strain Rate Sensitivity

    - Stress Relaxation & Creep

    - Cyclic Loading

    • Limited to uniaxial tests

    • Necessity to better understand the

    structural arrangement in the dermis

    TEM, SEM, Confocal Imaging…

    • Some more in-depth energy dissipative

    processes can be added

    -Friction

    -Shear-Lag [10]

    -Damage evolution [11,12]

    FEA, Molecular Dynamics.

    (resolution:512x512; frame rates: 10fps, 20fps, 80fps).

    The Matlab software Ncorr 2.1 [6] was used to perform DIC and estimate sample slipping.

    Experimental Results

    0

    2

    4

    6

    8

    10

    0 0.1 0.2 0.3 0.4

    Eng

    ineering S

    tress

    (MP

    a)

    Engineering Strain

    Loading/Unloading Tests

    16%

    35%

    40%

    Scanning Electron Micrograph of a Collagen Fiber in the dermis of

    pig skin

    The principal load-bearing component

    of skin is the dermis, composed of

    collagen (~30% v.f.) [7,8], elastin (~2%

    v.f.) [7,8] and a soft viscoelastic matrix.

    Collagen fibrils form bundles, which are

    initially crimped. We describe the

    waviness of the fibers using a semi-

    circular model [9], with:

    - 𝑟0: initial radius - 𝜔0: crimp angle- ℎ: fiber thicknessThe deformation of such a fiber is

    expressed by:

    𝜎 = න0

    𝜀𝑐

    𝐸𝑎𝑝𝑝(𝜀)𝑑𝜀

    Where 𝐸𝑎𝑝𝑝 is the apparent Young’s

    Modulus along the axis of tension, defined by the structural parameters listed above.

    𝜙𝑐

    𝜙𝑒

    Linear Elastic

    Neo-Hookean

    S-shaped Model

    Tensile Test of Pig Skin (Transverse) at 10-2s-1

    𝜂𝑔 = 100𝑀𝑃𝑎 ⋅ 𝑠

    Influence of the strain rate

    𝐸𝑐 = 136 𝑀𝑃𝑎𝑟0 = 8.9 𝜇𝑚𝜔0 = 54°𝐻𝑐 = 4 𝜇𝑚𝛾𝑐 = 17°𝐸𝑒 = 1𝑀𝑃𝑎𝜇𝑚 = 58 𝑘𝑃𝑎𝜂𝑚 = 7.46𝑒

    6𝑀𝑃𝑎 ⋅ 𝑠𝜂𝑔 = 4.65𝑒

    5 𝑀𝑃𝑎 ⋅ 𝑠

    Mesostructural Simscape ModelPeriodic Representative Volume Element in tension (Abaqus Finite Element Model)

    • Crimped Collagen Fibers spaced apart with a given distance

    • Embedded in a hyperelastic matrix Averaged Stress vs. Strain in the RVE for different

    values of µ (E=200GPa)

    TEM,SEM,

    SAXS…FEA

    Block Model

    Structural

    Arrangement

    Experiments

    Constitutive and Structural

    Parameters of Skin

    Interactions

    https://www.mathworks.com/products/simscape.htmlhttps://www.astm.org/Standards/D412http://ncorr.com/