structure ofkinkin buckle propagation on elasticpipeline€¦ · nonlinearity. ‘w'hne...
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Structure of kink in buckle propagation
on elastic pipeline
N Sugimoto
Depar咄ent of Mechanical Engineering, Fac141tyof Engineering Science,
University of osa㎞,0saka 560, 翔)an
Reprintedfrom ASME Book NO AMR137
1UTAM Symposium 爽NonlinearWaves in SOlids
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i
Structure of kink in buckle propagation on elasticpipeline
N Sugimoto
Z)9a?4mesi Q/4fecんa7z・icalj7り171ee7`1?1・,9,.Facs&yθ/'f7z夕i7z・eer17り・S'cie刄cej
ひy1‘i‘ue7`s≒ofosa・kG。 0sa,kG,560,J叩a'n・
This paPerconsiders麟eady buckle propagationon anelastic pipeline sl!bjected to
a combined action of bending, axial tensionand external hydrostatic side pressure.
A structu:re of a kink i芦examined by applying the idea of the ma,tched-asymptotic
expansion method to thenonnnear wave equations for the beam4exural mode coupled
with the ring-flexural mode derived previously. Their “outer solutions" are nothing but
theonesto the equations simpnfied 晦the approximation that the thecro8sgsectional
ovanzation bal゛"ces with the cirmumferential bending. Although they suggest
propagation of a kink,the appr(xximation becomes invalid at the very kink so that the
iuter solutions cannot be employed there. For the kink,“lnner solutions" aresought by
taking account of the lo4itudinal stretching as a shellin addition to the circumferential
bendhlg. lt then becomes possible to give the lowest innerstructure of the kink a・nd also
to provide u㎡formly valid solutions through6ut the pipenne. But a problem whether or
not the apPropriate outer solutions can be singled out stm remains unresolved.
INTRODUCTION
ltis known as the buckle propagation that when a subma・
rine pipeline is subjected toacombined action of bend-
ing, axial tension and hydrostatic side pressure exter-
nally,a buckle (i.e. a local khlk)can be propagated along
the pipenne, entailiilgits catastrophic conapse (Palmer
and Martin (1975),Mesloh ei al・ (1976)).lmportant
point is that itoccurs under the side Pressure even well
below the bucknng pressure of the pipe due to the side
pressure. lts phenolnenological aspect has beencla,rified
to some extent by the experiments due to Kyriakides and
Babcock(1981)and Kyriakides and Chang (1992),but
its physical mecha・nism for initiation and propagation of
the buckle has been left open.
This motivated the author to consider theoretically
such a very interesting phenomenon (Sugimoto(1987,
1989a,b)).Admittedly,both elasticand plasticbeha,vior
of the pipeline are engaged in highly nonlhlear manner.
But it is conjectured that the proPagation mechanism
associated globany with the pipenne wm be maintained
elasticany,whereas the plastic collapse wmensueafter
propagation of buckle so that the plasticitywm not take
part in the propagation mechanism. Focusing only on
the aspect of propagation, the formulation was given in
the framework of the thjree-dimensional theory of elas-
tic but finitedeformations to derive the nonlinear wa,ve
equations .forthe beam-flexural modecoupled with the
ring-flexural mode. While steady propagation of a kink
is suggested by the equationssimplified,the purposeof
this paper is toexamine an inner structure of the kink
by solving the fu,llequations.
ln the beginningμt is instructive to l?capitulate the
results wi仏in the elastic theory so far obtained. The
mechanism for steady propagation is found to be given
by the tension efrect due not only to the axial tension
applied externany but also to the side pressure. 'When
this tension eflectazld the bending balancefor the beam-
flexural mode, the ring・.flexuralmodecanbe simplified
into that the cross-sectionalovalization bal&nces with
the circumferential bendhlg. 'Wlth this simpnfication,in
passing,the Brazier efect can be described by the equa・
tions in a static case without the axial tension. As the
Brazier eflectis explained by the energy method (Calla-
dine(1983)),the present equations ca‘nprovide a new
approach based on the dynamical equations. The steady-
wave solutions to the simplmed equations suggest prop-
agation of a kink in the de皿ection. Further it is shown
that the propagation velocity and the“propagation pres-
sure" necessary for initiation of propaliation of the kink
agree quantatively with the experimental results in spite
of neglect of the plasticity・
At the kink,however,it is found that the above sim-
plmcation becolnesinvand so that those solutionsshould
not be employed there. T徊khlk appears to be so in an
axial scale much longer tha!l a typical length of a buckle.
‘W'hen this situation is viewed from a standpoint of the
matched-asymptotic expansion method (see,e・g.Nayfeh
(1973)),the solutions to the simplified equations corrre-
spond to“outer solutions" to the full equatigns, while
“inner solutions" provide a structure of the khlk now
to be solved by taking full account of the ring-flexural
mode. ln this connection,it is asked whether or not the
piecewise valid outer solutions separated by the kink can
be singled out by examing the inner solutions. But this
problem stm remains unresolved. lt is obvious that only
the lowest-order inner solutions in this paper are insu伍-
cient for this purpose.
parl ot Nonlinear waves in solids, edited by JL Wegner and FR Norwood
ASME Book NO AMR137 346 @1995 American Society ofMechanical Engineers
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GovERNING EqUATloNs
At the outset, we present the governing equations for
elastic buckle propagation derived previously by Sugl-
moto(1987, 1989a・).when the pipenne is subjected to
finite bending as a beam, it gives rise to the hlextensional
ovaJization of the cross-section due to the geometrical
nonlinearity. ‘W'hne this,in turn, reduces the moment of
1【lertiaof the cross-section, the cross-sectional deforma・-
tion is supported by the circumferential bending and the
longitudinal stretching ai a shell in addition to the a.xial
tension appned.
Denoting by λand j, respectively,the de旦ection of
the pipeline as a beam and thecoe伍cient of thesecond-
harmonic component of the ovalized contour decomposed
injtothe R)urier series with respect to the circumferential
angle of the cross-section,the goveming equations are
given in the Lagrangian formulation as fonows:
∂り1 .ga,2
ρ゜'・Iir十‾i‾
ρ0
∂2/
㎜
∂t2+
2
㎜∂z2
ぐr--‐L
1+
一
ぐ
四
--
3
㎜2
う ー
j p一R
∂2λ
㎜∂z2
ぎ-71,
3-
㎜ 5
(倣)2
1---.″
-
㎜
7・;z
∂2j.jlぐ
(2)
NONLINEAR WAVES IN SOLIDS 347
assmed to be of comparable order of o(Z″y3),while a
magnitude of r is comparable with pa・/ll・,i.e. 0(.&y2).
For steady-wa・ve solutions pi'opagating with a constant
velocity lj(>O),we look for ,j4.and ,Zr which depend on
z a"d t only though a combination z - ・ut.Normalizing
the variables by setting ,A/G =λ″-・d(z - ・ut)/1=ぐ,it
then fonows from Eqs (1)axld(2)that
9a
ぐL nり
一一
「qJ
う ー
3IN
+
1 d4j″ d2j″ 3
召‘司r‘りqF゛一5
ぐ 訃・====・’ 八‥`。
一一
j
3 4
with c=d2,A' 7dぐ2,9,=(1・2 -‘t・1)/ε2‘t・g,96=(1・2-
痙)/占いnd4=(e4/72)(1-gア2)(1 - p7‘P。)-1,where lJO
is the speed of the longitudinal waves given by ,/(j;/po),
whne lla and ‘u&are the speeds of waves associated with
the eflective tension and given, respectively,by・,ZCr,7po)
and ・ぴ(TI,7p,o).Equations(3)and(4)provide the basis
for the foUowing analysis.
PROPAGATION OF KINK
We begin the analysis with noting that ga and 9みare
very small by the assumption that 7/Z ajndpa7 Ek a;x:e
ofO(72).ln considering propagation of a kink, it wa,s
emphasized by Sugimoto (1989b)that gaC in Eq (3)must
not be neglected because it is the very eflect that balances
with the bending on the second term and drives the kink
forward.This balance occurs not over the a,xial scale ぐ
associated with the typical length l of the buckle, but
overa longer scale Z defined by l 9a l1/2 ぐ.Rewriting Eq
(3)in terms of Z, hl fact,two terms balajnce ea.ch other,
while the first two terms in Eq (4)are found to be of
O(qJ1,qaqb)a‘nd to be very s:mall compared with the last
term.Thus jy is givenapproximately as
ぎ=-S r!2. (5)
Substituting thisinto Eq (3),we have the single equa・
tion for C. Setting 9δC2/2=j,it is simpnfied to
(1一心-
AI -
㎜ 士
〃λ
1 ぐ /㎜
dZ
j2 十4(sgn9,)j=o
゜ぞ(1-1)‘μ・
(6)
∂z21
+
Za2∂43″
一一20 ∂z4
∂2Zμ
㎜ ∂z2
1
3Zll,*2
㎜ 5a4
with .ZEμ=j/a where z and t denote, resp ectively, the a.x-
ial coordinate along`the pipenne and the time, whne a,瓦
aTld h,*denote,reSpeCtiVely,the pipe゛S radlUS at the mid-
dlesurface,the pipe゛s thickness a7爽ldits“eflective thick-
ness" denned by h,7,ノ(1-(y2),cr the Poisson゛s ratio. With
the densitypo in the undeformed state and the‘Young゛s
modulus Z,p aJld pe represent, respectively,the hydro-
static side pressure and the bucknng pressure given by
pc=Z(ll・/a)3/[4(1-・72)].The side pressure also increa,ses
the a.xial tension in addition to the one 7 appUed exter-
nally through the “efrective tension" 7・lz(=7十pa/2瓦)
and 7あ(=7'十・pa75k)。
For the sake of simplicity, the higher-order eflect in
the “ovanzation" j∃μhas been neglected in Eqs (1)and
(2)because l B″lmust always be less tha.n unity by
the assumption that the pipe°s periphery doei not touch.
specmcany,zl″2/16"`d 53″/6 have already been dis-
carded in Eqs(1)"ld(2),respectively(see Sugimoto
(1989a)).Although the discard of the latter might seem
to be inco】!lsistent,itprovides the higher-order modmca・・
tion to the lowest nonlinear term on the right-hand side
of Eq (2)(i.e. of cubic order as a whole)so its neglect is
consistent with that oIB″2716in Eq (1)。
Here the fonowing points should bere:rna,rked.Deriva,・
tion of Eqs (1)aTld(2)rests on the scaling assump-
tion that the two small parameters ぞ(≡G,7 l≪1)and
7(≡瓦/a≪1),lbeing a typical axial length of the
buckle,satisfy the order relation 7 ~62. 1n addition,
a ma・gnitude of p is smaner than pc, of course, but p is
十j
㎜2/
・Wlth j。・‘1″and .Zμare derived as follows:
with j4q。j、Z6’
3’=一弘 (7) 9
Here the sign“士”inλ″indicates two possibnty of posl-
tiveornegative deflection,but only positive one iscon-
cerned in the following. The solutions to Eq(6)have al-
ready been obtained analyticaUy and discussed fully by
Sugimoto(1987).lt is found that two types of the solu-
tionsexist depending on the sign of ga,the“flexural wave
… 一 一
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348 NONLINEAR WAVES IN SOLIDS
mode” for ga >O and the“buckle propagation mode” for
ga<0. 0f course,the latter is concerned here.lnpartic-
ular,ifthe boundary conditions for the undeformed state
are applied at the i�inity of Z,j is given by the inverse
of the fonowing functions:
、/(2-f)一石tanh‾1・y(1-//2)-、zo=士z(8)
Here an integration constajnt Zo is taken to be Zo = 1-
(1/y2)tanh‾1(1/、/2)so as to set j=1 at the origin of
Z. The sign“士"indicates a palr of solutions symmetric
with respect to Z。
As the point / =1 is a shlgular Point of Eq (6)、dj/dぐ
diverges there. Since / represents physically thecross-
0.5
0.25
0
一2百
丿
一石’
l l l-1.0 -0.5 O
Z
0.5 1.0
FIG 1. ProjUes of the outer solutions for,the ddlection
λslnd the cross-sectional ovalization -jEI″as the func-
tion of the axial cooridnate Z (=19, 11/2 ぐ)where only
the subcritical bza,nches are ta,ken and the smaJl blank
circles represent the ki:akin the outer solutions.
0.5
0.25
-B3
2
㎜ l 竃 ,9
一一-F 9
- j
一ZO ZO
「
|
-1.0 -0.5 O Z
0.5
FIG 2. Profiles of the outel: solutions for the ddlection j,
s171dthe cross-sectional ovalization -j″&s the fllnction
of theaxial cooridna,teZ(=19, 11/2ぐ)where both the
sub- and. suPerczitical bra;xlchesareta,ken and the small
blank circles represent the kink in the outer solutions.
sectionalovalization jEμ,thedivergence of its derivatives
invalidates the neglect of the first two terms in Eq
(4)and therefore the aPproximation (5),nomatter how
small9a and 9ゐmay be.
Except for / =1,0f course,Eq(6)and therefore the
solutions(8)remaill to be vand approximately. Thus
(8)are to be interpreted as piecewise vand solutions for
O<j<1 and 1 </≦2,respectively. lt is reme:mbered
that the point / =1 corresponds to the nmit point of
the Brazier eflect,above which the static bending be-
comes unstable (see Sugimoto (1987)).ln view of this,
we call the solutions below j'=1 “SUbcritiCal braTlch",
while the ones above it the“supercritical branch"/Wlth
these two br゛-nches,we can buUd up any solution by com-
bining them appropriately so as to satisflythe bounda,ry
conditions at the infinity,for example, as shown in Figs
l and 2 (Sugimoto(1989b)).Among them, the solutions
consisting only of the subcriticalbranches in Fig l a・ppear
to be realized in reality.But it is emphasized that there
a.reno means to single out the appropriate solutions only
within the approximation based on Eq (6).ln any case,
a kink appears hl the deflection at j =1.
STRUCTURE OF KINK
Let us now consider inner solutions for a structure of
the kink by discarding the simplification. ″lothis end, it
must be the best if Eqs (3)and(4)could be solved fu.ny
without any approximation. But it is very di伍cult to do
so analyticiny and even numericany for very small values
of ga and 9&.By regarding ga and 9みas sman asymptotic
parameters,then, the idea of the matched-asymptotic
expansion method (called simply MAE hereafter)issuc-
cessfuny applicable.
lnnersolutions to Eqs (3)a・nd(4)are sought so as
to be matched asymptoticany with the outer solutions
(8).The matching conditions are given by expanding the
solutions(8)in terms of Z around Z =o. For example,
suppose that the subcritical outer solutiot1 / increases
from the minus infinity of Z to approach j 士1asZ→
o一(by taking the plus sign in (8)).Then the asymptotic
solutions as Z→O- are given by
/=1-21Z11/2十〇(z),
・・1'=町ざF7(1-11剔十〇(z2)),
RI=-
0
C -
㎜
l(1-21剔1/2十〇(z)),
(1- l z ll/2 十〇(z))・ (9)
一 一 一 一
、/2
㎜3φ
Here note that these expressions are also yand for the
subcriticalbranch with the minus sign in (8)asz→0十.
Accordhlg to the idea of MAE, the inhity asぐ→-(x)
corresponds to Z →O一 by assuming a suitable matchhlg
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0
一 一
regionand the inner solutions &re to besought so as to
approach asymptoticaUy the expressions (9)asぐ→-cx).
with z=19.11/2ぐsubstituted in (9),they contain the
small parameter l 9a l1/4. Thus it is 4ppropriate to seek
the innersolutions for j″ and C in the form of power
SerieS expaTlsion With reSpeCt tO 1 9a l1/4。
Then the lowest problem becomes
1一9″
㎜ 12
2 ぐE
d4召″
㎜ dぐ4
nり
一一
Tj a:1
eQIN
+
十j″十δC2=0,
where the・ term with ・gihi.s
(1o)
311一一
ぐ
been discarded because 9&
is of comparable order with ga. liot this problem, the
matching conditions are simply given as follows:
3・ -,一旦1
C→谷 asぐ→-(x).
Equation(10)can be immediately integrated,on
posing the matching conditions(12),togive
ト =
C
う p″
3一2
2φ
㎜9φ
(12)
lm一一
(13)
Using this relation to enminate C in Eq (11),we have
δ
㎜12
43″
㎜
dぐ4+
(3'十2/9)2(3'十8/9)
(3'十6/9)2
This equation can be integrated once into
δ
㎜12
L
dBl a3B’
一一-dぐdぐ3
ular solution:
ぐ1一2
差dぐ4
+
r .
j
=0
(j'十2/9)3
2(j'十6/9)
=0
(14)
-0,(15)
(16)
(17)
(18)
-β’
1.0
6一9
0.5
0
NONLINEAR WAVES IN SOLIDS 349
一
!
-
1.
£ ● ㎜ ●
|
f
t
| | |-3 0 -1.0
o aJ
1.0 2.0
2一9
-2.0
FIG 3. ProlUe of the ixlner solution for the cross-
sectional ovalization -3″ as the function ofぐwhere
δ`=2/9貪-7・d the blank circles represent the point
一召″=6/9.
-2.0
-0.4
LO
-1.0
-1.0
0
20.0
0
-0.8 -0 -
-20.0
-10.0
10.0
0
3.0
一
り一 j
_! 9
_2 9
l .|1.0
-O。8 -0.6 -0.4 0.2
盛
dζ
y
FIG 4. Trajectory of the inner solution l)r j″ pro-
jected in the plane (djEI″/dぐ,召″)where the blank
circlesrepzesent the point ,Z?″=-6/9.
d2.召″
皿 dぐ2
Where a・Tlintegration COnSta・nt haS been determined by
assuming that ぎ"`d its derivatiyes vanish asぐ→-(x).
Solutions around B″=-2/9
″lk)see゛71asymptotic behavior of jμasぐ→-(x〉,we
setjEI″=-2/9十&and substitute it into (14).Since
&vanishes as ぐ→-(x),we lhlearize the equation with
respect to &. But the resulting equation d4&/dぐ4=0
gives no inforn51ationthan &=0.Thus the linearization
is abandoned aTld the quadratiC term in &isretained as
4&㎜
dぐ4+a&2=0,
whereα=81/2δ.This equation has a non-trivial partic-
&=λ1ぐ‾4,
withλ1=-840/a=-560δ/27. ″lofind a general solu-
tion around it,we set &=λ1ぐ‾4十i;(ぐ)and substitute it
into Eq (16)to have
十験s十as2
包
dζ2
β'
FIG 5. Trajectory of the innex' solution for j″ Pro-
jected in the plue (d2j″/dぐ2,jEI')where d2 jEI″/dぐ2
diverges as j″→-6/9.
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350 NONLINEAR WAVES IN SOLIDS
Here we linearize Eq (18)a711d take a,n elementary solu-
tion in the form ofぐ″`,sbeing a const"`t. Then the
proper values of g are given by s =8,-5, 1.5 士iへ/39.75.
Among them, only the solution with g =-5 satisfiesthe
mat(ihing condition as ぐ→-(x).
We note that solutions to Eq (15)(axld therefore Eq
(16))anow azl arbitrary choic芦of the origin of ぐ.Thus
(17)may be taken as λ1(ぐーぐo)‾4,ぐo be1ロ,g an arbi-
・ j ・ ・trary constazlt. Maldng use of thii arbitraziness, &just
obtained can be absorbed into the solution (17)so that
&may be taken to be zero. From this,it is found that
(17)is the only asymptotic solution erna,nating from the
minus i�inity ofぐ.
Owing to this solution,we can now integrate the fuII
equation(15)numericany. ln doing so,the higher-oder
terms than (17)are included in the expansion as fonows:
=λ1ぐ‾4+λ2ぐ‾8+…, (19)
withλ2=-548800δ2/3159. Figure 3 shows -.Zr as the
function ofぐ.Here the fuU solution to Eq (15)is drawn
by taking δ=2/9 for definiteness (so that / =c2)・
Figures 4 and 5 show the projection of the trajectory of
the solution in the phase space (が,dy/dぐ,d2 B'7dぐ2).
The arrows indicate the dlrection of the solution startklg
fi'om BI=-2/9 at the minus i�inity ofぐtowardぐ=0.
Solutions around BI=-6/9
lt is found from these figures that the solution which has
started fi:om β″=-2/9 crosses j″=-6/9.As j?″ap-
proaches it,Figs 4"`d 5 show that dj″/dぐremains to
be finite but d2,ZI″/dぐ2tends to diverge. This is under-
stood from that the point .Z?″=-6/9 is a singular point
of Eq (14).ln view of the numerical results,we consider
゛71asymptotic solutionaroundj″=-6/9. Supposing
that lμcrosses-6/9 at a certain value ofぐ,sayぐ1jt is
suggested to be of the fbnowing form of the power series
combined with the logarithmic singularity:
RI十こ=μoξ十μ1ξ21og1 4 1十μ2ξ2十μ3ξ3(log lξ1)2十…・ 9
(2o)
with 4 =ぐーぐ1 where μo is ゛71 arbitray constantl
whneμ1=64/243δμg,μ2=352/729δμg and μ3=
4096/17714yδ2μg. The principle of advancing the expan-4096/1
● ●sion is to determinecoefncients of r(1og lξ1)゛-1(m,n:
positive integers)so as to satisflyEq (15)successively
from the lower oider terms toward the higher-oderones.
Asμo is arbitrary,this expansion may contain other ar-
bitrary const゛nts than μo. These constajntscannot be
specmed by such a local ajnalysisaloneand should be de-
termined globally hl co7`711ectionWith the matching con-
ditions.
Apart from this sohltion,wehave a,ngther asymptotic
solution around jr =-6/9. supposing that ,ZI″takes
-6/9 at a certain point ぐ=ぐ2,itis given in the form of
the power series of ?74/3as follows:
jy+;1=z/1 ?74/3+μ2 ?78/3+…lIIn
Z・
ぐ
with 77 =ぐーぐ2 where z/1=-(16/15δ)1/3 and z/2 =
(43740/343δ2)1/3.Beca,use the second-order deivative
diverges as ?7→0,wec"`not foUow (21)to solve Eq (15)
numericany. By trialand error in view of (21),however,
we can have a solution wh:ich tends to (21)as ?7→0,
while to the other asymptotic solution (20)as 77tends to
a finitevalue of ?7.1f Eq (15)is solved in η<0,then it
is possible to find such a sohltion that μo becomes con-
sistent with the one (μoQゴー1.310)already obtaixled for
the solution starting from 3″=-2/9. 1t shows that -RI
increases from 6/9 toward the negative direction of ?7to
attain the maximum -B″ Q;S0.735 and then returns to
6/9 from above at ?7 s -0.260. VVith this solution,we
ca71connect the solution startingfrom召″=-2/9 at the
minus innnity ofぐby adjusting the origin ofぐ.Further-
more since the solution (21)is symmetric with respect
to ?7=0,it can be continued i11to the positive region
of ?7 andeven connected beyond BI=-6/9 nkewise.
W'ith such continuation,the fun inner solution -,1ris
drawn with the a,xisof symmetry atぐ=O. Asぐtends to
the plus infinity,thissolution approaches asymptotically
j″=-2/9。
The curvature C of the deflection 。・47is easny calcu-
lated by (13).According to -jr <6/9 or -B″>6/9,
C is positive or negative, respectively,so that the de-
flectionis found to be convex downward or upward. 0f
course,the deflection can be obtained by integrating C
twice withrespect toぐ by using the matching conditions
(9).The curva,ture starts from y2/(3φ)at the minus
infinity ofぐ(note that this value is derived from the
qua・dratic term in z for the deflection in (9),though not
expncitly given there).From the matching conditions,
the deflection takes a very large value へ/2/(919al,,ノ6)
SlnCe 9a is sman. But the deflectionderived from (13)gives no more than the higher-oder modification. Thus
as far as the deflection is concerned, the outer solution
prevailsinto the kink to the lowest approximation.
DISCUSSIONS
The hmer solution in the kink has been obtained. But
it should berelnarked that as jr approaches -6/9, C
diverges as (13)suggests. Then the neglect of gaC in
Eq(3)is inadmissible and the solution just obtained be-
comes invalid i】lthe vicinity of the connection point. ln
this case, the fun equations (3)and(4)must be solved by
considering a further“inner region" around j″=-6/9in
the hlner solutions. ln the verycoreof this region,how-
ever,d23″/dぐ2 and y in (4)may be negl9cted because
the former exhibits the weak logarithmic singularity and
the latter is only just -6/9 as foUows:
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i
-19,1C十
1
1 2
一一2dξ2
d43″一一2o d£4
ぐE nり
一一
J-。
う ー
3一2
+
0
一一
C
3一5
+
Their exact solutions can be found as follows:
j″+4一3
一一 19, 1ξ2,1oglξ|十z)14十z)242,
C 一
一
、/(219.1)
3ξ ’
(22)
(23)
(24)
where Z)l and Z)2&re arbitrary constants to be deter-
mined in connection with the asymptotic solution (20)・
The solutions (24)are considered to give its hlner solu-
tionsat the very point ,ZEI″=-6/9.
solutions around(24),it win be possi
solutions th:rough j″=-6/9.
By gxpanding the
ble to connect the
CONCLUSION
R)r the stea・dy buckle propagationon anelastic pipeline。
the uniformly valid solutions have been obtained by ap-
plying the idea of the matched-asymptotic expansion
method to the governi】lgequations derived previous¥
The outer solutions suggest propagation of a kink in an
axial scale much longer than a typicallength of a buckle,
whne the inner solutions give the structure of the kink.
But it is stm open within the present lowest innersolu-
tions how the approPriate outer solutions canbe singled
out.
lnside of the kink, the cross-sectional ovalization is sup-
ported not only by the circumferential bending as in the
outer solutions but also the longitudinal stretching as a
shell.lt is found that the a,bsolute value of the ova,liza-
tion B″ txcetds beyond 2/9 as the critical vaJue given by
the Brazier eflect and attains the maximum value O。735
approximately. ln contrast with the outer solutions, the
eflective tensions a・nd the inertia do not play a primary
role except for the vicinity oIB’=-6/9. Around this,a
further inner structure appears where the curvature dl-
verges. These results are the very merit of the dynamical
equations(1)and(2)that cannot be described by the
NONLINEAR WAVES IN SOLIDS 351
energy method used in the Brazier eflect。
Fhlally itis concluded that propagation of a kink along
the pipenne can be explained even within the theory of
nonlinear elasticity.But the pipenne resumes its original
shape after the kink has been propaga・ted. Therefore, of
courselno coUapse can be covered by the present theory,
which is the inherent demerit. ″lbestabnsh a physical
mecha”is再nnking between propagation of a kink j゛-71d
ensuing plastic conapse seems to beavery di伍cult prob-
lem but a chanenging one.
ACKNO'VV'LEDGEIMIENT
The author wishes to thank ProfessorT. Kakutani for
his comments on the manuscript.
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