1. Trang chủ
  2. » Kỹ Thuật - Công Nghệ

ANALYTIC SOLUTIONS OF ELASTIC TUNNELING PROBLEMS Phần 4 doc

12 183 0
Tài liệu đã được kiểm tra trùng lặp

Đang tải... (xem toàn văn)

Tài liệu hạn chế xem trước, để xem đầy đủ mời bạn chọn Tải xuống

THÔNG TIN TÀI LIỆU

Thông tin cơ bản

Định dạng
Số trang 12
Dung lượng 107,68 KB

Các công cụ chuyển đổi và chỉnh sửa cho tài liệu này

Nội dung

An analytical solution for a deforming, buoyant tunnel in an elastic half-plane was derived in this chapter.. Chapter 5BUOYANCY OF A RIGID TUNNEL Buoyancy effects arise after the excavat

Trang 1

Section 4.2 Solution for a Deforming Hole in a Half-Plane 25

The expansion of the left-hand side of (4.24) is not as trivial, and will be

greatly simplified by multiplication with 1− ασ The right-hand side of the

modified equation can then be expanded as follows We write

G(ασ ) = 2µ(1 − ασ ) g h

m (ασ )= ∞

k=−∞

A k σ k (4.31)

where we have assumed that the given displacements along the hole, multiplied

by 2µ(1−ασ ), can be expanded into a Fourier series Such an expansion should

be possible for all problems of practical significance Note that the function

G(ασ )has same definition as in [42] The logarithmic terms in the right-hand

side of (4.24) can be expanded with help of the formula given in (3.7):

log 1

1− ζ =



n=1

ζ n

n , |ζ | < 1, (4.32) where the principle branch of the logarithm has been chosen The modified

form of (4.25) resulting from the multiplication with 1− ασ can be expanded

as follows (using (4.32) and the series in(4.31)):

(1− ασ ) g h

m(ασ )= ∞

k=−∞

Ak σ k (4.33)

where

Ak =

A k+

h

F x+ iF h y



1+ (α2− 1)k k(k − 1)α k



k ≤ −2,

A−1+α(

h

F x+ iF h y )

(2− α

2)ακ(

h

F x− iF h y )

4π(1 + κ) k = −1,

A0+ C Fα2(

h

F x+ iF h y )

h

F x− iF h y

4π(1 + κ) +κ(

h

F x− iF h y )

4π(1 + κ) (1− α2) k = 0,

A1− αC F+ακ(

h

F x+ iF h y )

h

F x− iF h y

4πα(1 + κ)

+α(κ − 1)(

h

F x− iF h y )

A2−α2κ(

h

F x+ iF h y )

h

F x− iF h y

A kκ(

h

F x+ iF h y )



α k k(k − 1)



k ≥ 3.

(4.34)

Trang 2

26 A Deforming Circular Tunnel Chapter 4

The expansion of the right-hand sides of both (4.21) and the modified form

of (4.24) is complete The left-hand sides of these equations can be expanded through substitution of (4.27) and (4.28), as mentioned before The details of these expansions, which are straightforward, are omitted here

Determination of the Laurent Coefficients

The unknown coefficients in the Laurent series (4.27) and (4.28) can be

de-termined by comparing the coefficients of like powers of σ in the expanded

boundary equations The results of these calculations for the expansion of (4.21) are

c0= B◦ 0− a0−1

2a1−1

c k = B−k − b k−1

2(k + 1)a k+1+1

2(k − 1)a k−1, k > 0, (4.36)

d k = Bk − a k+1

2(k − 1)b k−1−1

2(k + 1)b k+1, k > 0. (4.37)

These equations can be used to determine each of the coefficients c k and d k

once a k and b k have been determined Note that each of the coefficients c kand

d k are dependant on three levels of coefficients (e.g a k−1, a k , and a k+1)

Expressions for a k and b k are found by comparing the coefficients of like

powers of σ in the expansion of the modified form of (4.24) This results

in a complicated system of equations which are simplified considerably by

eliminating c k and d k through use of (4.35) – (4.37) Equations for a k+1and

b k+1are then obtained which are dependant on a single level of coefficients:

(1+ κα 2k+2)a

k+1+ (1 − α2)(k + 1)b k+1= α2(1+ κα 2k )a k

+ (1 − α2)kb k + α k+1A

k+1

+ Bk+1− α2Bk , k≥ 0 (4.38) and

α 2k (1− α2)(k + 1)a k+1− (κ + α 2k+2)b

k+1= α 2k (1− α2)ka k

− (κ + α 2k )b k + α k A−k + α 2k B−k − α 2k+2B

−k−1

, k ≥ 0, (4.39) where we have multiplied through by α k in order to make the expressions

numerically stable for large values of k.

Analytic Solution of the System

Equations (4.38) and (4.39) can be solved for a k and b knumerically, as suggested

in [42] We choose to solve the system analytically After some algebraic manipulation, which will not be given in full here, the solution is given by

a k+1=λ k11a k+λ k12b k+λ k13, (4.40)

b k+1=λ k21a k+λ k22b k+λ k23, (4.41)

Trang 3

Section 4.2 Solution for a Deforming Hole in a Half-Plane 27

where

k

λ11 =κα2+ [α22+ α2) + (1 − α2)2(k + 1)k + κα 2k+4]α 2k

k

λ12 =κα2− κ − (1 − α2) [(1 − α2)k + 1]α 2k

k

λ13 =(κ + α

2k+2)(B

k+1

− α2Bk ) + [α(κ + α 2k+2)A

k+1

]α k

κ + γ k α 2k

+(1− α

2)(k + 1)(A−k + α k B−k − α k+2B −k−1

)α k

k

λ21 =(1− α2) [α2− (1 − α2)k + κα 2k+2]α 2k

k

λ22 =κ + [1 + κ2α2+ (1 − α2)2(k + 1)k + κα 2k+2]α 2k

k

λ23 =(1− α

2)(k + 1)(α 2k+1A k+1

+ α k Bk+1− α k+2B k

)α k

κ + γ k α 2k

(1+ κα

2k+2)(A −k

+ α k B−k − α k+2B −k−1

)α k

with

γ k = (1 + κ22+ (1 − α2)2(k + 1)2+ κα 2k+4. (4.48)

Hereγ kandλ k mn , n are real andλ k mn , n = {3},is complex

Explicit Determination of the Coefficients

By studying the expanded expressions for the first few coefficients, it becomes

clear that explicit equations for a k and b kcan be written as follows:

a k =β k011a0+β k012a0+

k−1



i=0

k

β i13 k = 1, 2, 3, , (4.49)

b k =β k021a0+β k022a0+

k−1



i=0

k

β i23 k = 1, 2, 3, , (4.50)

where

k

β lmn=

l

k−1

λ mj

k−1

β k = l + 2, l + 3, l + 4, ,

(4.51)

Trang 4

28 A Deforming Circular Tunnel Chapter 4

with l = 0, 1, 2, , and where the summation convention (summation over like indices) has been adopted for the symbols λ and β, with m = 1, 2, n = 1, 2, 3, and j = 1, 2 Note that β k lmn , n β k lmn , n= {3} is complex

Determination of the Remaining Unknown Coefficient

It is apparent from these equations that the boundary conditions are not sufficient

to determine the last unknown, a0, as noted in [42] It can be seen from (4.49) – (4.50) and (4.35) – (4.37) that this unknown is incorporated in every coefficient

of the Laurent series (4.27) and (4.28) The value of a0affects the convergence

of the Laurent series; in fact, on the basis of (4.42) – (4.47) and (4.40) – (4.41),

a k and b k will each approach a constant value in the limit that k → ∞, the

value of which is determined by the starting value of the coefficients, a0 An

expression for a0can be determined by requiring that these constants tend to

zero as k → ∞, which is a necessary condition for the convergence of the Laurent series (4.27) and (4.28) along the outer boundarysof the annulus

Enforcing the condition that a k → 0 and b k → 0 as k → ∞ in the complex

conjugate of (4.49) and in (4.50) gives

0=∞β012a0+∞β011a0+∞−1

i=0

0=∞β021a0+∞β022a0+

∞−1

i=0

where we have used the notation

β lmn= lim

k→∞

k

β lmn , ∞ − 1 = lim

k→∞(k − 1). (4.54)

Solving the system (4.52) – (4.53) for a0results in

a0=

β012∞−1

i=0

β i23−∞β021∞−1

i=0

β i13

β021∞

β011−∞β022∞

β012

We note that (4.55) gives the proper result for the limiting case that there are

no resultant forces and no stresses or displacements given on either of the two

boundaries L s and L h In this case the expansion coefficients,BkandAk, are

equal to zero for every value of k By examining the terms of the form β ij3

it is apparent that the leading factor in these terms will always be of the form

λ j3, causing them to be zero when allBk and Ak are zero The conclusion is

that a0= 0 in this case, with the consequence that all of the coefficients vanish This corresponds to the case that there are no stresses and no displacements in the entire half-plane, which is a direct consequence of unloaded condition along the boundaries

Trang 5

Section 4.3 Chapter Summary 29

Final Form of the Transformed Solution

The final form of the solution in the z-plane is given by the potentials (4.1) and

(4.2) They can be expressed in terms of ζ through use of (4.7), (4.17), (4.27),

and (4.28) The result of the transformation is

ϕ

m (ζ )= −

h

F x+ iF h y

2π(1 + κ)

κ log(− i2a

1− ζ ) + log(−

i2aζ

1− ζ ) + a0+∞

k=1

a k ζ k+∞

k=1

b k ζ −k ,

(4.56)

and

ψ

m (ζ )=

h

F x− iF h y

2π(1 + κ)

log(− i2a

1− ζ ) + κ log(−

i2aζ

1− ζ ) + c0+∞

k=1

c k ζ k+∞

k=1

d k ζ −k ,

(4.57)

where the coefficients a k , b k , c k , and d k are given by (4.55), (4.49) – (4.50),

and (4.35) – (4.37), and where a is given by (4.8) These potentials, written

in terms of the transformed parameter ζ , can be used to compute the stresses

and displacements by conformally mapping the basic equations (2.1) - (2.5)

Details of the implementation have been included in Appendix B

An analytical solution for a deforming, buoyant tunnel in an elastic half-plane

was derived in this chapter The method used consists of first determining the

general form of the potentials for a half-plane with a hole, when a resultant force

on the hole due an excavation-related buoyancy effect is present The potentials

derived in Chapter 3 were used for this purpose, and it should be noted that

they contain two logarithmic terms each, yielding unbounded displacements at

infinity The half-plane region, the potentials, and the boundary equations were

then transformed to an annulus in order to facilitate an expansion in Laurent

series After the expansion of the potentials (excluding the logarithmic terms)

and the boundary conditions was performed, the unknown Laurent coefficients

were determined in an analytical limiting process

Trang 6

30 A Deforming Circular Tunnel Chapter 4

Trang 7

Part II

APPLICATIONS AND CONCLUSION

31

Trang 9

Chapter 5

BUOYANCY OF A RIGID TUNNEL

Buoyancy effects arise after the excavation of a tunnel due to an unloading of the material under the tunnel This can be understood mathematically by inte-grating the initial gravitational stresses around the circumference of the tunnel, which results in a force equal in magnitude to the weight of the excavated ma-terial (minus the weight of the tunnel lining) This force, which is referred to here as the buoyancy force, is represented in the solution of Chapter 4 by the resultant forceF h x+ iF h y acting on the tunnel In the mathematical idealization

of this problem all of the excavated material is removed instantaneously and simultaneously replaced by a tunnel lining of negligible, or zero, weight The resultant force acts on the tunnel in the instant after excavation, and vanishes through a combination of a vertical movement of the tunnel and an equaliza-tion of the stresses in the ground through deformaequaliza-tion This process results in equilibrium of the tunnel and an unloading of the ground The deformations and the final stresses acting on the tunnel lining are the focus of this chapter The buoyancy effect was included by Yu [45] in the solution for a completely rigid tunnel with a lining of negligible weight, excavated in an infinite plane In this solution a vertically varying gravitational field is applied to an elastic plane, but the effects of the free surface are ignored The buoyancy effect is also present

in the solution for the excavation of an unlined (and thus stress-free) tunnel in

an elastic half-plane by Mindlin [18] In his solution, Mindlin only obtained equations for the stresses and did not determine the displacements In addition

to these solutions, Verruijt [44] determined the approximate stresses acting on

a rigid, buoyant tunnel by assuming that the horizontal stresses directly above the tunnel, and the horizontal-vertical shear stresses in the entire field, are not affected by the excavation of the tunnel

When studying deep tunnels, a constant stress due to the overburden is often assumed, and the buoyancy effect is usually ignored (see for example [26, 8, 4]) For shallow tunnels, however, the approximation of a constant gravitational stress around the tunnel results in stresses along the nearby surface To cir-cumvent this, a more realistic gravitational loading with a vertically varying

33

Trang 10

34 Buoyancy of a Rigid Tunnel Chapter 5

gradient may be applied, making it necessary to include buoyancy effects in order to ensure equilibrium of the tunnel

In this chapter, we treat the simple case of a shallow tunnel with a circular liner of negligible weight which is perfectly rigid and which is bonded to the surrounding soil This will allow us to study the buoyancy effects in their simplest possible form The solution can be superimposed on the solutions for other deformation modes in later chapters in order to include the stresses induced by gravity on those solutions as well

The solution of a rigid tunnel in a heavy half-plane is composed of two parts: the solution for the stresses induced by gravity in the half-plane and the solution for the stresses and displacements induced by the resultant force acting on the tunnel due to buoyancy

In geotechnical engineering it is common to write the solution for the stresses induced by gravity as

where γ is the unit weight of the material and K0is the (constant) coefficient

of lateral earth pressure (K0is an independent parameter, determined by the geological history of the material) The displacements for this problem are deliberately left out, as we are only interested in deformations that occur after the material has been deposited [25]

The stresses and displacements induced by the resultant force acting on the tunnel can be obtained using the solution presented in section 4.2 There are two given components in this solution: the resultant force acting on the hole, and the boundary conditions along the tunnel

The resultant force is equal to the weight of the ground removed during excavation minus the weight of the tunnel lining In this solution, we neglect the weight of the tunnel lining, and it follows that the resultant force on the hole

in the solution of Chapter 4 can be written as

h

F x+ iF h y = iγ πr2, (5.4)

where r (as in Chapter 4) denotes the radius of the tunnel.

The boundary conditions for a rigid tunnel are that the displacements along the tunnel are constant This insures that the tunnel does not deform, but allows a certain amount of rigid body motion due to the rebound of the ground underneath the tunnel In this formulation of the problem the buoyancy force acting on the tunnel is known beforehand and is given by (5.4), but the amount of rigid

Trang 11

Section 5.1 Solution of the Problem 35

body motion of the tunnel is not Since an arbitrary rigid body motion can be

added to the solution for the displacements [23], zero displacements along the

tunnel boundary can be enforced without loss of generality (the actual boundary

condition along the tunnel periphery is that the displacements are constant)

Zero displacements along the tunnel are specified in the solution by setting

the given boundary functiong(z) h = 0 in (4.6) Consequently, the mapped

displacement function is also equal to zero:g h

m (ασ )= 0 It follows from (4.31) that

G(ασ ) = 2µ(1 − ασ ) g h

m (ασ )=



k=−∞

A k σ k = 0, (5.5)

from which it then follows that A k = 0 for all k The Fourier expansion given

by (4.34) can now be calculated by using these values for A k and by using the

value of the resultant force given by (5.4) This completes the solution for a

resultant force acting on a rigid tunnel The result is given by (4.56) and (4.57)

The results for this part of the solution can be normalized by setting the

parameter P in Appendix B equal to γ h2 It follows from (B.13) that the

expression for the resultant force (5.4) becomes

h

F x+ iF h y

P = iπ r

h

2

which is only dependant on the radius to depth ratio of the tunnel Since the

only component of the solution in Chapter 4 which is not dimensionless in this

case is the expression for the resultant force, it follows from the discussion

in Appendix B that dimensionless contours of the stresses and displacements

can be constructed which will only depend on the parameters r/ h and ν The

displacements will be given in terms of P /2µ = γ h2/( 2µ) and the stresses

will be given in terms of P / h = γ h, as can be seen from (B.24) – (B.26).

The solution for the gravitational stresses can be made dimensionless in a

similar fashion Multiplying the stresses (5.1) – (5.3) through by the same factor

h/P = 1/(γ h) as used above yields

σ xx

γ h =y

σ yy

γ h = K0

y

σ xy

Contours of the initial gravitational stresses generated from (5.7) – (5.9) will not

depend on the value of h if the x and y coordinates are normalized by division

by h, as will be done for the figures in this thesis.

In the following chapters the focus will be on plots of the incremental stresses

due to the deformation modes that are being analyzed (in this chapter those are

Ngày đăng: 07/08/2014, 04:21

TỪ KHÓA LIÊN QUAN