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MODELING OF CONCRETE MATERIALS AND STRUCTURES

Kaspar Willam, University of Colorado at BoulderIn cooperation with Bernd Koberl, Technical University of Vienna, Austria.

Class Meeting #6: Tension Softening vs Tension Stiffening

Smeared Crack Approach: Plastic Softening (isotropic case)

Axial Force Member in Tension and Compression: Snap-Back Effect

Cross-Effect: Lateral Confinement due Mismatch in 3-D

Tension Stiffening: Debonding in Reinforced Concrete

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING AND APPARENT DUCTILITY

Tensile Cracking:Smeared Crack Approach vs Plastic Softening.

Axial Force Problem:Serial Structure-Localization in Weakest Link.

Localization of Axial Deformation:Snap-Back and 3-D Cross-Effect when elastic energy release exceedsdissipation in softening domain.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING

Tensile Failure of Axial Force Member:

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

1-D PLASTIC HARDENING/SOFTENING

Elastic-Plastic Decomposition:

ε = εe + εp where εe =σ

E eand εp =

σ

Ep

Consequently,

ε =σ

E e+

σ

Ep=

σ

Etan

Elastoplastic Tangent Stiffness Relationship:

σ = Etanε where Etan =EeEp

Ee + Ep

Note: Etan = −∞when Ecrit

p = −Ee.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

3-D PLASTIC SOFTENING

Rankine Criterion for Tension Cut-Off: FR(σσσ, κ) = σ1 − ft(κ) = 0

Associated Plastic Flow Rule: εεεp = λmmm where εp1 = λ sign(σ1)

Isotropic Strain Softening Rule: ft(κ) = ft + Epκ where −E < Ep < 0.

Plastic Consistency: FR(σσσ, κ) = σ1 − Epκ = 0.

Strain-driven Format: from κ = εp1 = λ we find λ = E

E+Epε1

Tangent Stiffness Format: σ1 = E[ε1 − λ] = Etanε1 where Etan =EEp

E+Ep

Fracture Energy Based Softening:

Ep = dσ1dε

p1

= dσ1

dufN

dufN

dεp1

= Kp s

where s = crack separation

GIf =

∫ f

u σ1dufN = 1

2ft ufcr

Critical Softening:Ecrit

p = Kcritp s = −Ee

or Kcritp = −Ee

s

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

WEAK ELEMENT IN AXIAL FORCE MEMBER

Snap-Back Analysis of Serial Structure:

Static Equilibrium: ∆σaxial = ∆σe = ∆σs

Total Change of Length of Axial Force Member: ∆` = ∆`e + ∆`s

∆` =∆σe

Ee`e +

∆σs

Es`s

and

∆σaxial =EeEs

Ee`s + Es`e∆`

Controllable Softening Range as long as:

Ee`s + Es`e > 0

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING

Critical Size of Softening Zone for Snap-Back:

`crits = −Es

Ee`e

Note Snap-Back in spite of Constant Fracture Energy: Gf = const

0

1000

2000

3000

4000

5000

6000

0.0E+00 2.0E-05 4.0E-05 6.0E-05 8.0E-05 1.0E-04 1.2E-04

displacement [m]

forc

e [N

]

Gf = 100 NmLs=0,0095m=Ls,critGf = 100 NmLs=0.0448m>Ls,critGf = 100 NmLs=0.0077m<Ls,crit

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING

Cohesive Interface Approach: Strong Discontinuity

∆σ =KsEe

Ee + Ks`e∆` snap-back when `e

crit = 2EeG

critf

f 2t

Note: `ecrit compares with characteristic length of Hillerborg et al.

Effect of different Gf values on Structural Softening:

0

200

400

600

800

1000

1200

1400

0.00E+00 2.00E-05 4.00E-05 6.00E-05

displacement [m]

forc

e [N

]

Gf = Gf,crit = 34Nm

Gf = 32Nm < Gf,crit

Gf = 50Nm > Gf,crit

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING

Fracture energy-based softening: Linear vs Exponential Format

Mesh-size dependent softening modulus: Es = dσduf

duf

dεf= Kshel

0

1000

2000

3000

4000

5000

6000

0.00E+00 3.00E-05 6.00E-05 9.00E-05 1.20E-04

displacement [m]

forc

e [N

]

Gf=120Nm - linear softening DP Gf=120Nm - exp. softening DPGf=120Nm - linear softening - SC Gf=120Nm - exp. softening SC

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING

3-D Cross Effects: of Damage-Plasticity Model in Abaqus

Displacement Continuity introduces lateral confinement

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING

3-D Cross Effects Eliminated by Shear Slip and Loss of Bond

Insert zero shear interface elements between weak softening element and elasticunloading elements.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION SOFTENING

Cohesive Interface Elements Eliminate 3-D Cross Effects:

No lateral confinement due to loss of bond.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

MISMATCH AT PLASTIC SOFTENING-ELASTIC UNLOADING INTERFACE

• Perfect Bond: No Separation-Delamination:us

axial = ueaxial and us

lat = uelat with εs

lat = εelat

• Statics: σsaxial = σe

axial = σaxial

• Plastic Softening-Elastic Unloading in Axial Tension:

- Strain Rate in Plastic Softening Domain: εεεs = EEE−1s σσσ + εεεp

- Strain Rate in Elastic Unloading Domain: εεεe = EEE−1e σσσ

- Parabolic Drucker-Prager Yield Condition: F = J2 + αI1 − β = 0where α = 1

3[fc − ft] and β = 13fcft

- Associated Plastic Flow Rule: εεεp = λmmm = λ[sss + α111]

- Lateral Plastic Strain Rate: εlat = λmlat = λ[13(σslat − σaxial) + α]

• Elastic-Plastic Mismatch due Axial Tension:Introduces lateral contraction in softening domain:

σslat =

νsEe − νeEs

Ee(1− νs) + Ls

LeEs(1− νe)σaxial − λEe[

1

3(σs

lat − σaxial) + α]

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

BIMATERIAL INTERFACE CONDITIONS

Perfect Bond:

[|uN |] = ueN − us

N = 0 and [|tN |] = teN − ts

N = 0

Weak Discontinuities: all strain components exhibit jumps across interfaceexcept for εe

TT = εsTT restraint.

Note: Jump of tangential normal stress, σeTT 6= σs

TT .

Imperfect Contact:

[|uN |] = ueN − us

N 6= 0 whereas [|tN |] = teN − ts

N = 0

Strong Discontinuities: all displacement components exhibit jumps acrossinterface.

Note: FE Displacement method enforces traction continuity in ‘weak’ senseonly, hence [|tN |] 6= 0.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

COMPRESSION SOFTENING

Issue of Material vs Structural Response:

Axial Force Member: compression response of weak element

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

COMPRESSION SOFTENING

Full 3-D Cross Effect:

Lateral confinement introduces uniform triaxial state of stress (elastic if no cap)

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

COMPRESSION SOFTENING

3-D Cross Effect: Confinement Introduces Elastic Triaxial Compression

No softening of Damage-Plasticity Model in Abaqus because of missing cap.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

COMPRESSION SOFTENING

Reduction of 3-D Cross Effect:

Cohesive Interface Elements: eliminate lateral confinement

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

COMPRESSION SOFTENING

Cohesive Interface Elements Eliminate 3-D Cross Effects

Localization of compression failure in weak element.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

COMPRESSION SOFTENING

Snap-Back due Localization of Compression Failure in Weak Element

Cohesive Interface elements eliminate lateral confinement.

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Stress Transfer of Parallel System: Full Bond

Kinking iff embedded rebar has no shear and bending stiffness

(Avg: 75%)PE, PE33

+6.352e−06+5.290e−03+1.057e−02+1.586e−02+2.114e−02+2.643e−02+3.171e−02+3.699e−02+4.228e−02+4.756e−02+5.285e−02+5.813e−02+6.341e−02

1

2

3

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Stress Transfer of Parallel System: Full Bond

Mesh Effect for Constant Fracture Energy: Gf = const.

0

5000

10000

15000

20000

25000

30000

35000

40000

45000

0 0.0004 0.0008 0.0012 0.0016 0.002

displacement [m]

forc

e [N

]

single - rebar

1x1 Gf=32Nm

4x4 sym Gf=32Nm eq.ef=0.0026 [-]

8x8 sym Gf=32Nm

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Stress Transfer of Parallel System: Full Bond

Mesh Effect for Constant Cracking Strain: εf = const.

0

5000

10000

15000

20000

25000

30000

35000

40000

45000

0 0.0004 0.0008 0.0012 0.0016 0.002

displacement [m]

forc

e [N

]

single rebar

1x1sym ef=0.0026 [-]

4x4 sym ef=0.0026 [-] eq. Gf=32Nm8x8 sym ef=0.0026 [-]

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Stress Transfer of Parallel System: Full Bond

Regular crack spacing ‘independent’ of mesh size.

(Avg: 75%)PE, PE33

+6.352e−06+5.290e−03+1.057e−02+1.586e−02+2.114e−02+2.643e−02+3.171e−02+3.699e−02+4.228e−02+4.756e−02+5.285e−02+5.813e−02+6.341e−02

1

2

3

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Local Study of Stress Transfer in Segment between Adjacent Cracks:

Effect of fracture energy mode II for modeling shear debonding.

0

5000

10000

15000

20000

25000

30000

35000

40000

45000

0 0.00025 0.0005 0.00075

displacement [m]

forc

e [N

]

GfII = 10xGfI

GfII = GfI

naked steel

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Stress Transfer of Parallel System near Center Crack

Shear transfer in steel rebar (von Mises)

(Avg: 75%)S, Mises

+6.000e+04+6.133e+04+6.267e+04+6.400e+04+6.533e+04+6.667e+04+6.800e+04+6.933e+04+7.067e+04+7.200e+04+7.333e+04+7.467e+04+7.600e+04

+0.000e+00

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Stress Transfer of Parallel System near Center Crack

Shear transfer in concrete (von Mises stress)

(Avg: 75%)S, Mises

+0.000e+00+5.833e+01+1.167e+02+1.750e+02+2.333e+02+2.917e+02+3.500e+02+4.083e+02+4.667e+02+5.250e+02+5.833e+02+6.417e+02+7.000e+02+7.600e+04

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

TENSION STIFFENING

Stress Transfer of Parallel System near Center Crack

Axial stress transfer at steel-concrete interface

4.30E+084.40E+084.50E+084.60E+084.70E+084.80E+084.90E+085.00E+085.10E+085.20E+085.30E+08

0 0.03 0.06 0.09 0.12 0.15

length of the specimen [m]

stre

ss in

reba

r[N/m

²]

0.00E+00

5.00E+05

1.00E+06

1.50E+06

2.00E+06

2.50E+06

3.00E+06

3.50E+06

4.00E+06

4.50E+06

stre

ss in

con

cret

e[N

/m²]

SM of rebar S33 of concrete

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

CONCLUDING REMARKS

Main Lessons from Class # 6:

Tension Softening vs Tension Stiffening:Both Serial and Parallel Systems Exhibit Snap-Back Conditions.

Loss of Bond at Weak Element Interface:Loss of Triaxial Confinement-No Cross Effects

Loss of Bond at Steel-Concrete Interface:Tensile Cracking Followed by Shear Debonding

Class #6 Concrete Modeling, UNICAMP, Campinas, Brazil, August 20-28, 2007

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