T˚ij = Lijkl(T, e) Dkl+ Nij(T, e)||D|| (A.1) Lijkl = fbfe
tr ( ˆT2)
³F2δikKδjlK+ a2TˆijTˆkl´ (A.2)
Nij = fbfefda F tr ( ˆT2)
³Tˆij + ˆTij∗´ (A.3)
Tˆij = Tij
tr T (A.4)
Tˆij∗ = ˆTij − 1
3δijK (A.5)
a =
s3 8
(3 − sin ϕc)
sin ϕc (A.6)
F =
vu ut1
8tan2ψ + 2 − tan2ψ 2 +√
2 tan ψ cos (3θ) − 1 2√
2 tan ψ (A.7) tan ψ = √
3|| ˆT∗|| (A.8)
cos (3θ) = −√
6 tr ( ˆT∗3)
·
tr ( ˆT∗2)
¸3/2 (A.9)
130
fd =
oedometric compression tests and drained triaxial tests is shown in the following diagrams (Fig. A.1 to A.5). The conclusions of this parametric study are summarized in Table A.1.
0.4 0.5 0.6 0.7 0.8 0.9 1 1.1
0.001 0.01 0.1 1 10
e
p’ in MPa
hs=95 MPa n=0.10 n=0.20 n=0.25 n=0.30 n=0.40 n=0.50 n=0.60
0.4 0.5 0.6 0.7 0.8 0.9 1 1.1
0.001 0.01 0.1 1 10
e
p’ in MPa
n=0.50 hs= 10 MPa hs= 50 MPa hs= 95 MPa hs=150 MPa hs=200 MPa hs=300 MPa hs=500 MPa
Figure A.1: . Influence of hs and n on the oedometric compression lines calculated with Eq. (2.2).
0
Figure A.2: Influence of a variation of hs on (a) deviatoric stress q and (b) volumetric strain εv during drained triaxial shearing (ID,0 = 0.88) and (c) oedometric compression lines (ID,0= 0.27 and ID,0= 0.79).
0
Figure A.3: Influence of a variation of n on (a) deviatoric stress q and (b) volumetric strain εv during drained triaxial shearing (ID,0 = 0.88) and (c) oedometric compression lines (ID,0= 0.27 and ID,0= 0.79).
0
Figure A.4: Influence of a variation of α on (a) deviatoric stress q and (b) volumetric strain εv during drained triaxial shearing (ID,0 = 0.88) and (c) oedometric compression lines (ID,0= 0.27 and ID,0= 0.79).
0
Figure A.5: Influence of a variation of β on (a) deviatoric stress q and (b) volumetric strain εv during drained triaxial shearing (ID,0 = 0.88) and (c) oedometric compression lines (ID,0= 0.27 and ID,0= 0.79).
Parameter Major Influence Minor Influence Drained Triaxial Shearing
α max (q) εpeak1 := ε1(max (q)) shear stiffness dq/dε1 dq/dε1(ε1 << εpeak1 ) εv
Oedometric Compression negligible
Drained Triaxial Shearing β dq/dε1(ε1 < εpeak1 ) max (q)
ε1(max (q)) εv
Oedometric Compression initial bulk modulus (dp0/dV ) dense samples loose samples hs, n on everything none
Table A.1: Summary of the parametric study.
A.2.1 Mathematical Formulation
˚T = fbL :ˆ ³D − Dvis´ (A.18)
fb = −βbtr T (A.19)
βb = 1
(1 + a2/3)κ (A.20)
L =ˆ ³F2I + a2T ˆˆT´ (A.21)
Dvis = −DrB OCR~ −1/Iv (A.22)
B =~
õF a
¶2³
T + ˆˆ T∗´+ ˆT : ˆT ˆT∗− ˆT ˆT : ˆT∗
!→
(A.23)
OCR = pe/p+e (A.24)
pe = pe0·
µ1 + ee0 1 + e
¶1/λ
(A.25) p+e = p
1 +
à q Mp
!2
(A.26)
p = −trT/3 (A.27)
q =
s3
2||T∗|| (A.28)
T∗ = T + p · 1 (A.29)
M(T) = 6F (T) sin ϕc/(3 − sin ϕc) (A.30)
A.2.2 Grain Size Distributions
100 90
80
70
60
50
40
30
20
10
10063206.32.00.630.20.060.020.0060.0020.001 98765432198765432198765432198765432198765432
Percent Finer by Weight
Grain Size d in mm Clay SiltFine−Medium−Coarse− SandFine−Medium−Coarse− GravelFine−Medium−Coarse− Cob. Hydrometer AnalysisSieve Sizes Grain Size Distribution
110154158159160162472578
Figure A.6: Grain size distributions of the investigated materials.
of undrained triaxial tests and oedometric compression tests is shown in the following diagrams (Fig. A.7 to A.11). The conclusions of this parametric study are summarized in Table A.2.
Figure A.7: Influence of a variation of λ on (a) stress path in the p–q plane, (b) volumetric strain εvvs. axial strain ε1and (c) excess pore water pressure ∆u vs. axial strain ε1during undrained triaxial shearing and (d) on oedometric compression lines.
0
Figure A.8: Influence of a variation of κ on (a) stress path in the p–q plane, (b) volumetric strain εvvs. axial strain ε1and (c) excess pore water pressure ∆u vs. axial strain ε1during undrained triaxial shearing and (d) on oedometric compression lines.
0
Figure A.9: Influence of a variation of βRon (a) stress path in the p–q plane, (b) volumetric strain εvvs. axial strain ε1and (c) excess pore water pressure ∆u vs. axial strain ε1during undrained triaxial shearing and (d) on oedometric compression lines.
0
Figure A.10: Influence of a variation of Iv on (a) stress path in the p–q plane, (b) volu-metric strain εv vs. axial strain ε1 and (c) excess pore water pressure ∆u vs. axial strain ε1 during undrained triaxial shearing and (d) on oedometric compression lines.
0
Figure A.11: Influence of a variation of ϕc on (a) stress path in the p–q plane, (b) volu-metric strain εv vs. axial strain ε1 and (c) excess pore water pressure ∆u vs. axial strain ε1 during undrained triaxial shearing and (d) on oedometric compression lines.
Parameter Major Influence Minor Influence Undrained Triaxial Shearing
λ —
Oedometric Compression dp0/dV(virgin load.) —
Undrained Triaxial Shearing
κ dq/dε1 —
d∆u/dε1 ∆u(ε1,u)
Oedometric Compression dp0/dV(unload./reload.) —
Undrained Triaxial Shearing
βR qu( ˙ε1) —
∆u(ε1,u) d∆u/dε1
Oedometric Compression
—
Undrained Triaxial Shearing
Iv q( ˙ε1) ∆u
Oedometric Compression
creep —
relaxation
Undrained Triaxial Shearing ϕc qu( ˙ε1)
∆u(ε1,u)
Oedometric Compression
— e100
Table A.2: Summary of the parametric study.
Material mR mT R βχ χ 110 7.0 7.0 10−4 0.10 1.0 154 7.0 7.0 10−4 0.10 1.0 159 7.0 7.0 10−4 0.03 1.0 160 7.0 7.0 10−4 0.05 1.0 162 7.0 7.0 10−4 0.10 1.0 472 7.0 7.0 10−4 0.10 1.0 578 7.0 7.0 10−4 0.10 1.0
Table A.3: Intergranular strain parameters of the investigated materials.
A.2.5 Interrelations between Parameters and/or Index Quanti-ties
Undrained Strength Ration
Material a b
110 0.408 0.939 154 0.323 0.948 158 0.301 0.906 159 0.282 0.957 160 0.262 0.932 162 0.405 0.967 472 0.356 0.971 578 0.316 0.955 Table A.4: Parameters a and b.
Appendix B
Benchmarking of CPT Interpretation Methods for Calcareous Sands
147
100 90 80 70 60 50 40 30 20 10 10063206.32.00.630.20.060.020.0060.0020.001
98765432198765432198765432198765432198765432
Percent Finer by Weight
Grain Size d in mm
ClaySilt Fine−Medium−Coarse−Sand Fine−Medium−Coarse−Gravel Fine−Medium−Coarse−Cob.
Hydrometer AnalysisSieve Sizes
Grain Size Distribution M000 M015 M030 M060 M100
Figure B.1: Grain size distributions of the investigated materials.
Test p0 K e ID qc,m kc qc,c
in kPa in % in MPa in MPa
M0-1 39 0.20 0.83 13 1.0 1.05 1.0
M0-2 77 0.41 0.81 18 1.8 1.06 1.9
M0-3 151 0.44 0.81 18 4.0 1.07 4.3
M0-4 226 0.46 0.82 17 5.5 1.06 5.8
M0-5 38 0.21 0.70 51 4.5 1.19 5.4
M0-6 149 0.47 0.69 52 12.7 1.20 15.2
M0-7 230 0.49 0.69 53 17.8 1.20 21.4
M0-8 41 0.26 0.66 61 5.5 1.24 6.8
M0-9 79 0.41 0.61 77 18.5 1.31 24.2
M0-10 157 0.50 0.65 64 18.7 1.25 23.3
M0-11 224 0.51 0.66 63 23.5 1.24 29.2
M15-1 43 0.57 0.90 -8∗) 1.5 1.00 1.5
M15-2 77 0.53 0.90 -7∗) 2.0 1.00 2.0
M15-3 147 0.50 0.90 -7∗) 4.0 1.00 4.0
M15-4 226 0.50 0.89 -5∗) 6.0 1.00 6.0
M15-5 44 0.53 0.75 40 4.8 1.12 5.4
M15-6 77 0.58 0.75 41 7.3 1.12 8.2
M15-7 146 0.53 0.73 48 13.8 1.14 15.8
M15-8 222 0.55 0.73 46 20.0 1.14 22.7
M15-9 27 0.49 0.69 59 13.0 1.18 15.3
M30-1 80 0.50 0.64 81 20.5 1.20 24.7
M30-2 80 0.50 0.77 43 10.9 1.10 12.0
M30-3 80 0.50 0.96 -14∗) 2.2 1.00 2.2
M30-4 143 0.50 0.64 81 26.5 1.20 31.9
M30-5 150 0.50 0.77 43 17.5 1.10 19.3
continued on the next page
∗) void ratio is greater than emax from standard laboratory tests
continuation
Test p0 K e ID qc,m kc qc,c
in kPa in % in MPa in MPa
M60-1 80 0.50 0.72 76 17.8 1.15 20.4
M60-2 80 0.50 0.81 54 12.5 1.10 13.8
M60-3 150 0.50 0.72 76 22.5 1.15 25.9
M60-4 150 0.50 0.81 54 17.0 1.10 18.8
M100-1 51 0.38 1.16 13 2.2 1.03 2.3
M100-2 73 0.35 1.16 14 3.3 1.03 3.3
M100-3 146 0.43 1.11 25 5.3 1.05 5.6
M100-4 218 0.46 1.14 17 8.5 1.04 8.8
M100-5 39 0.29 0.94 60 3.8 1.13 4.2
M100-6 72 0.48 0.98 53 5.6 1.12 6.2
M100-7 76 0.40 0.96 56 7.4 1.12 8.3
M100-8 143 0.42 0.97 54 13.5 1.12 15.1
M100-9 221 0.43 0.98 53 9.8 1.12 10.9
M100-10 43 0.26 0.74 104 24.3 1.24 30.1
M100-11 79 0.42 0.75 102 24.3 1.24 30.0
M100-12 155 0.47 0.82 87 27.0 1.20 32.3
∗) void ratio is greater than emax from standard laboratory tests
Table B.1: CPT calibration chamber testing programme with initial conditions and re-sults.
where
- p0 = −2σr0 + σv0
3 is the effective mean pressure, - K = σ0r/σv0 is the principal stress ratio,
- e is the void ratio,
- ID = emax− e
emax− emin is the relative density,
- qc,m is the measured cone penetration resistance, - kc is the correction factor and
- qc,c= kc· qc,m is the corrected cone penetration resistance.
performed on the same specimen.
• The results shown in Figures B.4, B.5 and B.6 are the same as in Figures B.7, B.8 and B.9. The latter show the influence of the mean pressure, whereas the others show the influence of density on the cone penetration resistance.
-1.2
Figure B.2: CPT results: Material M0.
-1.2
Figure B.3: CPT results: Material M15.
-1.2
Figure B.4: CPT results: Material M30.
-1.2
Figure B.5: CPT results: Material M60.
-1.2
Figure B.6: CPT results: Material M100.
-1.2
Figure B.7: CPT results: Material M30.
-1.2
Figure B.8: CPT results: Material M60.
-1.2
Figure B.9: CPT results: Material M100.
B.3.1 Laboratory and Post Test Calculation Results
Figure B.10: Oedoemeter tests, material M0.
0
Figure B.11: Drained triaxial test, material M0.
0.4
Figure B.12: Oedoemeter tests, material M15.
0
Figure B.13: Drained triaxial test, material M15.
0.4
Figure B.14: Oedoemeter tests, material M30.
0
Figure B.15: Drained triaxial test, material M30.
0.4
Figure B.16: Oedoemeter tests, material M60.
0
Figure B.17: Drained triaxial test, material M60.
0.4
Figure B.18: Oedoemeter tests, material M100.
0
Figure B.19: Drained triaxial test, material M100.
Material ϕc hs n ed0 ec0 ei0 α β
[◦] [MPa]
M0 32,0 175 0,57 0,551 0,844 0,971 0,11 1,4 M15 32,0 135 0,57 0,579 0,859 0,988 0,10 1,5 M30 32,0 58 0,55 0,618 0,948 1,090 0,17 2,0 M60 35,1 45 0,55 0,653 1,014 1,166 0,15 1,7 M100 37,7 95 0,50 0,762 1,223 1,406 0,13 1,1 Table B.2: Material parameters of the hypoplastic constitutive model.
0
Figure B.20: SCE simulation results: Material M0 and M15.
0
Figure B.21: SCE simulation results: Material M30 and M60.
0 1 2 3 4 5 6
0 0.05 0.1 0.15 0.2 0.25 0.3 pLS in MPa
p0 in MPa
ID 0%
10%
20%
30%
40%
50%
60%
70%
80%
90%
approx.
Figure B.22: SCE simulation results: Material M100.
Material a1 a2 a3 b1 b2 b3
M0 1,1324 -8,5289 -1,7739 0,8241 0,1398 -1,4058 M15 1,1423 -8,4150 -1,9256 0,8199 0,1403 -1,4478 M30 -0,4736 -9,8444 -2,1577 0,8793 0,2403 -1,4867 M60 -0,2468 -9,9956 -2,28278 0,8735 0,2481 -1,5327 M100 0,7716 -8,0177 -1,9006 0,8666 0,1958 -1,5013
Table B.3: Parameter ai and bi for the approximation by Eq.(3.6) of the SCE simulation results (curves in Fig. B.20 to B.22).
Cudmani Schmertmann (cal.)
Mat. ∆ ∆max ∆ > 20%¯ Mat. ∆ ∆max ∆ > 20%¯
M0 11% 23% 3/11 M0 2% 6% 0/11
M15 26% 49% 6/9 M15 14% 32% 4/9
M30 34% 46% 5/5 M30 10% 37% 1/5
M60 32% 37% 4/4 M60 1% 1% 0/4
M100 11% 21% 1/12 M100 7% 18% 0/12
DIN Schmertmann (1976)
Mat. ∆ ∆max ∆ > 20%¯ Mat. ∆ ∆max ∆ > 20%¯
M0 17% 44% 4/11 M0 11% 19% 0/11
M15 14% 29% 1/9 M15 28% 50% 9/9
M30 9% 18% 0/5 M30 25% 32% 3/5
M60 7% 13% 0/4 M60 18% 25% 1/4
M100 19% 48% 5/12 M100 9% 21% 1/12
Table B.4: Benchmarking of the applied interpretation methods.
0
Figure B.23: Test vs. interpretation method after German Code DIN 4094.
0
Figure B.24: Test vs. interpretation method after Schmertmann (calibrated).
0
Figure B.25: Test vs. interpretation method after Schmertmann (1976).
0
Figure B.26: Test vs. interpretation method after Cudmani.
Appendix C
A CPT Interpretation Method for Clayey Soils
167
C.1.1 Test facility
Figure C.1: Left: Top plate and inner guiding pipe. Right: Top end of the inner guiding pipe with lip seals.
C.1.2 Sample Preparation and Installation
Figure C.2: Soil mixing device.
Figure C.3: Placement of the soil in the supported rubber membrane.
Figure C.4: Soil sample before and after preconsolidation.
-0.8
Figure C.5: Results of test #01 on brick clay.
-0.9
Figure C.6: Results of test #02 on brick clay.
-0.6 -0.5 -0.4 -0.3 -0.2 -0.1
0 0 0.25 0.5 0.75
z in m
qt in MPa
-0.6 -0.5 -0.4 -0.3 -0.2 -0.1
0 0 0.02 0.04 0.06 0.08
z in m
fs in MPa
-0.6 -0.5 -0.4 -0.3 -0.2 -0.1
0 0.48 0.49 0.5
z in m
u in MPa u2
Figure C.7: Results of test #03 on brick clay.
C.2.1 FE CPT Simulations
Material #110 #154 #158 #159 #160 #162 #472 #578
a 4.64375 3.28294 2.73169 2.43525 2.33153 5.1949 3.98272 3.97845 b 0.8539 0.82263 0.78716 0.77825 0.78765 0.88168 0.86754 0.883 Table C.1: Model parameters a and b of the investigated materials for the interpretation of CPTU results.
C.2.2 Numerical Determination of the Cone Factor N
ktMaterial #110 #154 #158 #159 #160 #162 #472 #578
a 11.3728 10.1611 9.0640 8.6487 8.8963 12.8293 11.2006 12.5802 b -0.0854 -0.1251 -0.1185 -0.1784 -0.1440 -0.0858 -0.1039 -0.0720 Table C.2: Model parameters a and b for the determination of the cone factor.
8.50 9.00 9.50 10.00 10.50 11.00 11.50 12.00 12.50 13.00
0.04 0.06 0.08 0.10 0.12 0.14
a
λ
8.00 8.50 9.00 9.50 10.00 10.50 11.00 11.50 12.00 12.50 13.00
0.00 0.01 0.02 0.03
a
(a) κ (b)
8.50 9.00 9.50 10.00 10.50 11.00 11.50 12.00 12.50 13.00
0.30 0.40 0.50 0.60 0.70
a
ϕc in rad
(c) Figure C.8: Cone factor: Correlation between parameter a and (a) λ, (b) κ and (c) ϕc.
7.50
0.20 0.30 0.40 0.50 0.60 0.70 0.80
a
0.00 0.10 0.20 0.30 0.40 0.50
a
0.00 0.20 0.40 0.60 0.80 1.00
a
(c) CC (d)
Figure C.9: Cone factor: Correlation between parameter a and (a) wL, (b) wP, (c) IP and (d) the clay content CC.
−0.18
−0.16
−0.14
−0.12
−0.10
−0.08
−0.06
0.04 0.06 0.08 0.10 0.12 0.14
b
λ
−0.18
−0.16
−0.14
−0.12
−0.10
−0.08
−0.06
0.00 0.01 0.02 0.03
b
(a) κ (b)
−0.18
−0.16
−0.14
−0.12
−0.10
−0.08
−0.06
0.30 0.40 0.50 0.60 0.70
b
ϕc in rad
(c) Figure C.10: Cone factor: Correlation between parameter b and (a) λ, (b) κ and (c) ϕc.
−0.18
−0.16
−0.14
−0.12
−0.10
0.20 0.30 0.40 0.50 0.60 0.70 0.80
b
wL
−0.18
−0.16
−0.14
−0.12
−0.10
0.10 0.20 0.30
b
wP
(a) (b)
−0.18
−0.16
−0.14
−0.12
−0.10
−0.08
−0.06
0.00 0.10 0.20 0.30 0.40 0.50
b
IP
−0.18
−0.16
−0.14
−0.12
−0.10
−0.08
−0.06
0.00 0.20 0.40 0.60 0.80 1.00
b
(c) CC (d)
Figure C.11: Cone factor: Correlation between parameter b and (a) wL, (b) wP, (c) IP and (d) the clay content CC.
C.2.3 Application Example
−50
−45
−40
−35
−30
−25
−20
−15
−10
0.8 1.0 1.2 1.4
z in m
e b=0.83 a=3 a=4 a=5 a=6 in situ
−50
−45
−40
−35
−30
−25
−20
−15
−10
0.8 1.0 1.2 1.4
z in m
e a=5 b=0.75 b=0.80 b=0.85 in situ
(a) (b)
Figure C.12: Influence of a variation of the model parameters on the interpretation results.
Deep Vibratory Compaction
D.1 Sensitivity Analysis: Results
178
0.55
Figure D.1: Influence of ed0, ec0 and ei0 on the temporal change of e during the vibro compaction simulation.
0.60 0.65 0.70 0.75 0.80
0 5 10 15 20 25 30 35 40
e
t in s
36.3°
0.60 0.65 0.70 0.75 0.80 0.85 0.90
0 5 10 15 20 25 30 35 40
e
t in s
r2 = 1.00 m 29.7°
33.0°
36.3°
0.60 0.65 0.70 0.75 0.80 0.85 0.90
0 5 10 15 20 25 30 35 40
e
t in s
r3 = 2.00 m 29.7°
33.0°
36.3°
Figure D.2: Influence of ϕc on the temporal change of e during the vibro compaction simulation.
0.60
Figure D.3: Influence of n on the temporal change of e during the vibro compaction simulation.
0.60 0.65 0.70 0.75 0.80
0 5 10 15 20 25 30 35 40
e
t in s
0.11
0.60 0.65 0.70 0.75 0.80 0.85 0.90
0 5 10 15 20 25 30 35 40
e
t in s
r2 = 1.00 m 0.09
0.10 0.11
0.60 0.65 0.70 0.75 0.80 0.85 0.90
0 5 10 15 20 25 30 35 40
e
t in s r3 = 2.00 m
0.09 0.10 0.11
Figure D.4: Influence of α on the temporal change of e during the vibro compaction simulation.
0.60
Figure D.5: Influence of β on the temporal change of e during the vibro compaction simulation.
Two further Applications of Viscohypoplasticity
E.1 An Open Cut: Contract D-8, Chicago Subway
184
Figure E.1: [13].