5.2 Models for soil-pipe interaction analysis
5.2.1 Model neglecting soil-pipe interaction
Pipe is assumed to be much softer than soil and cannot provide any resistance to ground motions. Hence, the pipe perfectly conforms to free-field ground motions, which are the soil displacements induced by the propagation of seismic waves in the absence of excavation and structures. The free-field ground motions can be computed by either analytical solutions or numerical simulations.
5.2.1.1 Rayleigh surface wave in a homogeneous half-space by analytical expression
Letπ is the angular frequency, ππΌ, ππ½, and ππ are the phase velocities of compressional, shear, and Rayleigh waves, respectively. ππΌ = π/ππΌ, ππ½ = π/ππ½, and ππ = π/ππ are the corresponding wavenumbers. The displacements along x and y axes of Rayleigh surface wave, denoted asπ’π₯ andπ’π¦, are expressed as (Viktorov,1967)
π’π₯ = π΄ ππ πππ π¦β 2ππ π π π2
π +π 2
π
ππ π π¦
!
sin(ππ π₯βππ‘) , (5.1)
π’π¦ =βπ΄ππ πππ π¦β 2π2
π
π2
π +π 2
π
ππ π π¦
!
cos(ππ π₯βππ‘) , (5.2)
where A is an arbitrary constant,ππ = q
π2
π βπ2
πΌ, π π =q π2
π βπ2
π½, andπ‘is time.
5.2.1.2 Rayleigh surface wave in a heterogeneous half-space by finite element simulation
For basin configuration, the harmonic Rayleigh surface wave propagates from left to right, originates from stiff soil (soil 2) and reaches softer soil (soil 1). The reflection at the basin circumference and the wave interference inside the basin make the problem become more complex. The free-field ground motions inside the basin can be computed by FE analyses.
Ξ
eΞ
u
0bu
0eRayleigh O
y
x C
Figure 5.2: Geometry of the truncated domain with boundariesΞandΞe.
In FE analyses, the effective input forces are defined as equivalent input forces which are applied to generate a predetermined displacement field. We used the domain reduction method proposed by Bielak et al. (2003) to compute the effective input forces of the predetermined Rayleigh surface wave displacement field of soil 2. The configuration of the truncated domain is shown in Fig.5.2. The effective input forces π·effb and π·effe applied on
the boundariesΞandΞeat each time step are governed by
π·effb =βπ΄beπΒ₯0eβπ²beπ0e, (5.3) π·effe =π΄ebπΒ₯0b+π²ebπ0b, (5.4) where π΄be and π΄eb are the off-diagonal quadrants of the mass matrices assembled from the single layer of finite elements between two boundariesΞand Ξe, and π²be and π²eb are the off-diagonal quadrants of the corresponding stiffness matrices. For lumped mass, π΄be and π΄eb would be zero. π0bandπ0e are the predetermined displacement vector of nodes on ΞandΞe, respectively.
The Fourier transform of an unwindowed sinusoidal function with frequencyπis non-zero only at Β±π. However, for the FE analyses, we consider the signal only within a finite interval of time while implying zero values outside that time interval, which is equivalent to multiplying the waveform with a rectangular function, leading to the spectral leakage phenomenon. It is therefore necessary to use a windowing technique to distribute the leakage spectrally, allowing interesting features of the signal to be observed. Moreover, the tapering property of the window function prevents numerical artifact induced by a sudden application of non-zero value of signal at the beginning of the FE analyses. The π-point Tukey (a.k.a tapered cosine) window technique is used in this study, defined by
π€(π‘) =




ο£²




ο£³ 1 2
1+cos 2π
πΌ
(π‘βπΌ/2) , for 0β€ π‘ <
πΌ 2
1, for πΌ
2 β€ π‘ <1β πΌ 1 2
2
1+cos 2π
πΌ
(π‘β1+πΌ/2) , for 1β πΌ
2 β€ π‘ <1
(5.5)
whereπ‘ is an π-point linearly spaced time vector. The parameter πΌis the ratio of cosine- tapered section length to the entire window length, henceforth taken asπΌ=0.5.
0 0.5 1 1.5 2
-0.5 0 0.5 1 1.5
0 0.5 1 1.5 2 2.5 3
-0.015 -0.01 -0.005 0 0.005 0.01
ux uy
Figure 5.3: Displacements of Rayleigh waves as a function of: (a) depth; and (b) time.
The pattern of the Rayleigh wave displacements is illustrated in Fig.5.3(a). The displace- ment amplitudes Λπ’π₯ and Λπ’π¦, normalized with Λπ’π₯0, are plotted as a function of dimensionless depth |π¦|/ππ , where Λπ’π₯0 is the amplitude of x-displacement at the ground surface π¦ = 0 andππ =2π ππ /πis the wavelength of Rayleigh wave. Fig.5.3(b) shows time histories of the displacement components at the point (π₯ , π¦) = (0,0), which are the multiplication of harmonic Rayleigh wave in Eqs. (5.1), (5.2) and Tukey window in Eq (5.5).
The x- and y-components of the vectorsπ0
bandπ0e are predetermined with Eqs. (5.1), (5.2), and (5.5). We consider the Rayleigh wave propagates along the positive x-axis, starting at pointπ(0,0). Because of the finite wave velocity,π’π₯ andπ’π¦ at a point are zero when the waves have not reached that point yet, i.e., whenπ‘ < ππ π₯/π.
We wrote a subroutine incorporated into LS-DYNA solver to generate the Rayleigh surface wave propagation. The fidelity of this subroutine was verified for a case of Rayleigh wave propagating through a homogeneous elastic half-space soil domain, where analytical solution is available via Eqs. (5.1), (5.2), and (5.5). The input parameters for the verification problem are as follows: π =2πrad/s; the Poissonβs ratio, mass density, and shear modulus of soil domain are π = 0.25, π = 1800 kg/m3, and π = 4.5 MPa, respectively; and the scalar π΄ in Eqs. (5.1) and (5.2) is π΄ = 0.5193. For FE analysis, the number of elements per wavelength is chosen as ππ π π€ =50, while the time step size is based on the Courantβ
FriedrichsβLewy condition.
0 2 4 6 8 10 12
-0.05 0 0.05
ux Analytical u
x FE u
y Analytical u y FE
0 2 4 6 8 10 12
-0.05 0 0.05
ux Analytical u
x FE u
y Analytical u y FE
Figure 5.4: π’π₯andπ’π¦computed by analytical solution and by FE approach with incorporated subroutine: (a) at pointπ(0,0); and (b) at pointπΆ(125,0).
Fig.5.4 shows the displacements at two pointsπ andπΆ, computed by analytical solution via Eqs. (5.1), (5.2), and (5.5), and by FE approach with incorporated subroutine. The results by these two approaches agree well with each other. Meanwhile, Fig.5.5illustrates the displacement field contours of Rayleigh surface wave propagation at time π‘ = 7.25 second. Observably, for bothπ’π₯andπ’π¦, the wave envelopes travel from left to right without
Figure 5.5: π’π₯ andπ’π¦ displacement fields atπ‘ =7.25 s.
dispersion, which is expected for fundamental mode of Rayleigh wave in homogeneous elastic half-space soil medium.
5.2.2 Model considering soil-pipe interaction with free-field input The reduced-order model for SPI analysis is shown in Fig.5.6, in which the pipe is modeled as beam elements1 and the surrounding soil is replaced by a set of springs and dashpots formulated to represent its macroscopic reaction to differential deformations between soil and pipe.
The spring stiffness and dashpot coefficient per unit length along x-axis, ππ₯ and ππ₯, and along y-axis,ππ¦ andππ¦, are computed as
πj =< πΎjj
, (5.6)
πj == πΎjj
/π , (5.7)
1In the context of this chapter, a beam element refers to a beam-column element that resists both axial force and bending moment. Each node of the beam has one rotational and two translational degrees of freedom.
u
gyu
gxy
x c
yk
yk
xc
xFigure 5.6: Schematic of pipe analysis.
where j = x or y, < and =represent the real and imaginary parts. The SIFs along axial and vertical directions, πΎxx and πΎyy, were computed previously in Chapters 3and 4as a function of excitation frequencyπ, shear modulus and Poissonβs ratio of soil domain, burial depth and radius of the buried pipe.
The free-field ground motionsπ’π₯
π andπ’
π¦
π, obtained in the same way as in Subsection5.2.1, are applied at the ends of springs and dashpots as seismic excitation. The analysis was performed using OPENSEES framework.
5.2.3 Models based on substructure and finite element methods