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Meso-Mechanical Modeling of Canonical Perforation Experiments · •Meso-mechanical plain weave...

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Enterprise for Multi‐scale Research of Materials Meso-Mechanical Modeling of Canonical Perforation Experiments Christopher S. Meyer (UD/CCM, ARL), Bazle Z. (Gama) Haque (UD/CCM), John W. Gillespie, Jr. (UD/CCM), Daniel J. O’Brien (ARL), Enoch Bonyi (MSU), Kadir Aslan (MSU) How We Fit Technical Approach Key Accomplishments Key Goals Major Results Impact Materials-by-Design Process Ongoing and Future Work Mechanism-based Approach UNCLASSIFIED UNCLASSIFIED Experiments to see mesoscale damage mechanisms: matrix cracking, tow-tow debonding, tension-shear tow failure Modeling & simulation to understand mesoscale damage mechanisms Meso-mechanical model to capture mechanisms occurring at mesoscale: Transverse cone wave speed Transverse tow cracking Tow-matrix and tow-tow debonding Model damage and failure modes from understanding of mechanisms Demonstrated that at mesoscale, there is a perforation energy difference depending on impact location relative to a unit cell Damage characterization at microscale showed damage evolves from transverse matrix cracks to tow-tow delamination cracks Demonstrated characteristic patterns of mesoscale damage that relate to the mechanisms of damage formation: Transverse cracks – x pattern – tension in primary tows transferred to transverse tows 45° cracks – ◊ pattern – shear between orthogonal tows cracks interstitial matrix pockets Tow-tow delamination – + pattern – delamination of overlap between primary tows in tension and transverse secondary tows Found quantity of mesoscale damage increases with increasing impact velocity up to ballistic limit then decreases (localizes) with velocity Collaboration: Experiments (tension and impact): ARL, UD/CCM Damage mapping, characterization, visualization: MSU, ARL, UD/CCM Microscale modeling and model inputs: JHU, UD/CCM Uncertainty quantification: JHU, UD/CCM Meso-mechanical modeling: Develop mesoscale test method for tow-tow delamination traction- separation for model input properties Quasi-static and dynamic impact testing for model validation Impact experiments for through-thickness deformation wave propagation and effect on mesoscale damage modes and energy dissipation Build mesoscale model to better predict energy dissipation and damage over continuum model, validate with experimental data: Tension and Punch-shear (transverse cracking, tow-tow delamination) Impact (deformation wave propagation, back-face deflection, impact vs. residual velocity) In materials-by-design framework, use model to evaluate novel composite material systems and lead to enhanced soldier protection and lethality Macroscopic damage modes dissipate energy through Elastic strain energy (wave motion, vibration), plasticity Meso- and micro-mechanical damage mechanisms: Matrix cracking, debonding, tensile fiber fracture, etc. Isolate mechanisms that lead to damage modes (“See It”) Single layer eliminates delamination mode, interlaminar stress field, nesting Focus on perforation phase (eliminate penetration and transition) Isolate and characterize tension and shear damage modes and energy dissipation Characterize elastic wave propagation and effect on mesoscale damage modes and energy dissipation Systematically build up complexity of models (“Understand It”) Homogenized continuum with plain weave properties Meso-mechanical plain weave model geometry with cohesive zones bonding constituents Refine meso-model in terms of delamination response and transverse matrix cracking by evaluating/optimizing cohesive zone formulation, bilinear traction-displacement behavior, and predefined fracture planes Conduct tension testing 2-in wide single-layer PW tensile specimens, determine quasi-static tensile strength distribution, use DIC to identify strain levels at which transverse matrix cracks initiate and proliferate Demonstrate state-of-the-art continuum model (MAT_162) cannot adequately capture low-velocity VI-VR curve and transverse deformation wave propagation / back-face deflection Develop test methodology and specimens for determining quasi-static tow- tow delamination load-displacement behavior using punch-shear fixture, also conduct higher-rate drop testing to determine dynamic tow-tow delamination behavior for rate-dependent model inputs Develop test methodology and test specimens for determining quasi-static transverse crack load-displacement behavior using Keyence microscope and micro-tension test fixture In collaboration with ARL, conduct low velocity impact experiments of single-layer PW specimens large enough to measure transverse deformation cone wave velocity and back-face deflection Model the quasi-static and dynamic responses to validate meso-model Tensile testing of single-layer plain weave composite: experiments toward determining tensile strength distribution for model validation and UQ input preliminary meso-mechanical model results show more realistic tensile response than continuum UNCLASSIFIED Spcmn Width (in) E T (GPa) P2S1 1 12.477 P2S2 3 13.194 P2S3 3 13.650 P2S4 1 13.282 P4S5 2 13.543 P4S6 2 14.720 P4S7 2 13.887 0 100 200 300 400 500 600 0 0.01 0.02 0.03 0.04 0.05 Stress, MPa Strain P2S1 P2S2 P2S3 P2S4 P4S5 P4S6 Validated meso-mechanical plain weave composite model will be applied to woven composites of interest to the Army In materials-by-design framework, model will be used to evaluate novel composite material systems in ballistic impact leading to enhanced protection for the soldier Journal publications: Meyer et al., Mesoscale Ballistic Damage…, Intl J Impact Engineering 113, 2017 Bonyi, Meyer, et al., Quantification of Ballistic Impact Damage, Intl J Damage Mechanics, 2018. experimental tensile response experimental tension mesoscale strain response (DIC) transverse cracks tow-tow delamination 45° matrix cracks Continuum model reproduces experimental results above V BL ≈ 175 m/s, not at or below Preliminary meso-model results with tow-tow delamination indicate model is approximating energy dissipating delamination and sliding between tows, but need experimental results to provide correct tow-tow delamination cohesive parameters Preliminary model results also indicate strain localization at high velocity and strain concentrations in transverse tows where we expect to see transverse cracking, need experimental crack properties and cohesive crack placement continuum impact model V I -V R preliminary impact model with tow-tow delamination preliminary impact model with tow-tow delamination V I = 186 m/s V I = 472 m/s continuum tensile response Continuum tension model cannot capture mesoscale strain response
Transcript
Page 1: Meso-Mechanical Modeling of Canonical Perforation Experiments · •Meso-mechanical plain weave model geometry with cohesive zones bonding constituents •Refine meso-model in terms

Enterprise for Multi‐scale Research of Materials

Meso-Mechanical Modeling of Canonical Perforation Experiments

Christopher S. Meyer (UD/CCM, ARL), Bazle Z. (Gama) Haque (UD/CCM), John W. Gillespie, Jr. (UD/CCM), Daniel J. O’Brien (ARL), Enoch Bonyi (MSU), Kadir Aslan (MSU)

How We Fit Technical Approach Key Accomplishments

Key Goals

Major Results

Impact

Materials-by-Design Process

Ongoing and Future Work

Mechanism-based Approach

UNCLASSIFIED

UNCLASSIFIED

• Experiments to seemesoscale damagemechanisms: matrixcracking, tow-towdebonding, tension-sheartow failure

• Modeling & simulation tounderstand mesoscaledamage mechanisms

• Meso-mechanical model tocapture mechanisms occurringat mesoscale:

• Transverse cone wave speed• Transverse tow cracking• Tow-matrix and tow-tow

debonding

• Model damage and failuremodes from understanding ofmechanisms

• Demonstrated that at mesoscale, there is a perforation energy differencedepending on impact location relative to a unit cell

• Damage characterization at microscale showed damage evolves fromtransverse matrix cracks to tow-tow delamination cracks

• Demonstrated characteristic patterns of mesoscale damage that relate tothe mechanisms of damage formation:• Transverse cracks – x pattern – tension in primary tows transferred to

transverse tows• 45° cracks – ◊ pattern – shear between orthogonal tows cracks

interstitial matrix pockets• Tow-tow delamination – + pattern – delamination of overlap between

primary tows in tension and transverse secondary tows• Found quantity of mesoscale damage increases with increasing impact

velocity up to ballistic limit then decreases (localizes) with velocity

Collaboration: • Experiments (tension and impact): ARL, UD/CCM• Damage mapping, characterization, visualization: MSU, ARL, UD/CCM• Microscale modeling and model inputs: JHU, UD/CCM• Uncertainty quantification: JHU, UD/CCMMeso-mechanical modeling:• Develop mesoscale test method for tow-tow delamination traction-

separation for model input properties• Quasi-static and dynamic impact testing for model validation• Impact experiments for through-thickness deformation wave propagation

and effect on mesoscale damage modes and energy dissipation• Build mesoscale model to better predict energy dissipation and damage

over continuum model, validate with experimental data:• Tension and Punch-shear (transverse cracking, tow-tow delamination)• Impact (deformation wave propagation, back-face deflection, impact vs.

residual velocity)• In materials-by-design framework, use model to evaluate novel composite

material systems and lead to enhanced soldier protection and lethality

• Macroscopic damage modes dissipate energy through• Elastic strain energy (wave motion, vibration), plasticity• Meso- and micro-mechanical damage mechanisms:

• Matrix cracking, debonding, tensile fiber fracture, etc.• Isolate mechanisms that lead to damage modes (“See It”)

• Single layer eliminates delamination mode, interlaminar stress field, nesting• Focus on perforation phase (eliminate penetration and transition)• Isolate and characterize tension and shear damage modes and energy

dissipation• Characterize elastic wave propagation and effect on mesoscale damage modes

and energy dissipation• Systematically build up complexity of models (“Understand It”)

• Homogenized continuum with plain weave properties• Meso-mechanical plain weave model geometry with cohesive zones bonding

constituents

• Refine meso-model in terms of delamination response and transversematrix cracking by evaluating/optimizing cohesive zone formulation,bilinear traction-displacement behavior, and predefined fracture planes

• Conduct tension testing 2-in wide single-layer PW tensile specimens,determine quasi-static tensile strength distribution, use DIC to identifystrain levels at which transverse matrix cracks initiate and proliferate

• Demonstrate state-of-the-art continuum model (MAT_162) cannotadequately capture low-velocity VI-VR curve and transverse deformationwave propagation / back-face deflection

• Develop test methodology and specimens for determining quasi-static tow-tow delamination load-displacement behavior using punch-shear fixture,also conduct higher-rate drop testing to determine dynamic tow-towdelamination behavior for rate-dependent model inputs

• Develop test methodology and test specimens for determining quasi-statictransverse crack load-displacement behavior using Keyence microscopeand micro-tension test fixture

• In collaboration with ARL, conduct low velocity impact experiments ofsingle-layer PW specimens large enough to measure transversedeformation cone wave velocity and back-face deflection

• Model the quasi-static and dynamic responses to validate meso-model

Tensile testing of single-layer plain weave composite:• experiments toward determining tensile strength

distribution for model validation and UQ input• preliminary meso-mechanical model results show

more realistic tensile response than continuum

UNCLASSIFIED

Spcmn Width (in) ET (GPa)P2S1 1 12.477P2S2 3 13.194P2S3 3 13.650P2S4 1 13.282P4S5 2 13.543P4S6 2 14.720P4S7 2 13.887

0

100

200

300

400

500

600

0 0.01 0.02 0.03 0.04 0.05

Stre

ss, M

Pa

Strain

P2S1P2S2P2S3P2S4P4S5P4S6

• Validated meso-mechanical plain weave composite model will be applied towoven composites of interest to the Army

• In materials-by-design framework, model will be used to evaluate novelcomposite material systems in ballistic impact leading to enhancedprotection for the soldier

Journal publications: • Meyer et al., Mesoscale Ballistic Damage…, Intl J Impact Engineering 113, 2017• Bonyi, Meyer, et al., Quantification of Ballistic Impact Damage, Intl J Damage

Mechanics, 2018.

experimental tensile response

experimental tension mesoscale strain response (DIC)

tran

sver

se c

rack

s

tow

-tow

del

amin

atio

n

45°m

atrix

cra

cks

• Continuum model reproduces experimental results above VBL ≈ 175 m/s, not at or below• Preliminary meso-model results with tow-tow delamination indicate model is

approximating energy dissipating delamination and sliding between tows, but needexperimental results to provide correct tow-tow delamination cohesive parameters

• Preliminary model results also indicate strain localization at high velocity and strainconcentrations in transverse tows where we expect to see transverse cracking, needexperimental crack properties and cohesive crack placement

continuum impact model VI - VR

preliminary impact model with tow-tow delamination

preliminary impact model with tow-tow delaminationVI = 186 m/s VI = 472 m/s

continuum tensile response

Continuum tension model cannot capture mesoscale

strain response

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