PLANE ELASTIC-PLASTIC WAVES (0 PLOSKOI UPRUQO-PLASTICHESKOI Phfhf Vol. 29. No. 3, 1965,
VOLNE)
pp. 509515
A.M. SKOBEEV (Moscow)
(Rccaivcd
The problem equations
of oblique
proposed
the elastic
case
plicit
correspond
Problems either
of soil
of material
A study
and transverse
the solution
dynamics stress
that
satisfies
the
is made of motions
waves.
of the problem
of the cubic
result
of the problem,
from which
0 (El is found. has been
which
If the shear
can be written
[l]
in principle,
to describe
in
modulus
and
down in es-
model
are no solutions of the present adopted
1. Let We will
can clearly
problem
an entirely different
has
The experimental law has not been
tested
for testing
solved
Grigorian’s
by Antsiferov
for soil,
they obtained.
an elastic-plastic
lie in the boundary
7
=
and ffz*
halfspace plane
t/z @YU -
(J**),
of the stress
out in [6] led
test.
the equa-
be pointed
[?I. However,
of the present
along
there
The results
It should
system
is directed
II, and v are the velocities
at least
at all, since
and an associated
paper
K = p. dp / dp
are
of coordinates.
into the interior.
the x- and y-axes,
tensor,
to
proposed
the regrettable
carried
model.
and the results
and the x-axis
are components
one,
and Rakhmatulin
u (p),
it leads
However.
to be put to experimental
model
notation:
test
Hooke’s
which
(Jry, ‘Jyy
enables However,
is
symmetry
because
p (E).
different
use the following
CXX, z =
model motion.
the relation
T. The model
and the function
be used
in the
a stricter
condition available
heen
This soil
from those
us consider
The y- and z-axes
equations
the medium. tested.
tensor
the symmetry
complications stress
p ia a
of the stress
condition problem
on the shear
elastic-plastic
thoroughly
that generalizes
paper
significant
to describe
an arbitrary
of these
out that a similar significantly
involves
that the relation
can be obtained
By considering
of the present
form of the plasticity
of this
condition).
from the plasticity
This
relation
as in [2 - 51, that the pressure
one can derive
can be used
fact is that it has not been to a concrete
the assumption This
and that the secondinvariant
not only on E but also
by Grigorian
making
6 is given.
In the formulation
adopted.
the fact that u depends
8 alone
(the plasticity
formulation
solved
or by assuming,
dilatation
of the pressure
condition
are usually
u and the strain
as an experimental
a function
fJ =
composed
is investigated.
to longitudinal
are constant,
the nniaxial
function
they
[l]
28, 1964)
form.
between
tions
on a halfspace
by Grigorian
dp/dp
the quantity
impact
November
and
600
A.M. Skobssv
The following
i.e.,
on the
problem
boundary
y or I, the required We will
will
be considered
u (8) and 7(t) quantitiee
assume
are step
that the quantity
the eonva&ive
terms
to the solution
of the system
functions.
are o (x, t), 7(x,
in the equation
Assuming
that nothing
depends
on
t), and y (x, t).
1 - pe/p
is small
of Grlgorfan
in comparison
can be neglected,
with unity.
Then,
and the problem
leads
of equations
(1.1)
&G’+P_-+$-_-_-__ au with
the above-formulated
been
obtained
P
boundary
and initial
u ? %
at in (1.1) has
ap .LKap
and the continuity
at
(1.2)
equation 6$+&o
(1.3)
F (p) and h were determined
The quantities
in [I].
/p
If the shear cases tions
aqnation
the generalized
in system
Hooke’s
law,
F (p) is an experimentally The pressure
construct
conditions.
Let
in the theory (1.1)
determined
in Fig. some us write
the characteristics
occurs
plastically,
A = 0, and system
is the equation plasticity
to depend
then A > 0
(1.1) then reduces
; in the other
to the usual
equa-
of elasticity.
and the third equation
p is assumed
is shown
2. We will By definition,
aP
T‘he third equation
5 = p.
FIG. 1
p (p) relation
2F (P)
conditions.
J
The first
F’(P)
ax
F(P)
from the relation
f
initial
av
z
F (PI 8%
of motion,
the second
is the plasticity
equation
condition,
is
where
function.
on p and the direction
of the process.
A typical
1. solutions
of system
out the equations of a system
(1.1)
without
attempting
for the characteristics
of first-order
differential
to satisfy
of system eqaations
the
(1.1). are
Plane
curves
x - f (t) having
the following
the syatem are given on such uniquely
defined.
w given
elortic-pltutic
Denoting
properties
a curve,
: if all the unknown
the derivatives
differention
601
wavea
along
of these
the cwve
function9
functiona
f by d/t%,
will
appearing
ln
not be
for an arbitrary
fanction
on f we have (2.1)
System rivatives
(1.1)
contains
of the type (2.1). derivatives Thus, which
the six unknown8
are to be determined Since
the resulting
can be determined the condition
u, v, u, 7,
by the ten equation8 system
uniquely
p, and
of system
is linear
f(t)
partial
de-
and by ten equation0
in the partial
when the determinant
for the characteristics
y; the twenty
(1.1)
derivatives,
all the
is nonzero.
ia the vanishing
of this
determinant,
haa the form
dx 0 0 0 0 0 0 0
dt 0 0 0 0 dx dt. 0 0 0 0 dx 0 0 0 0 0 0 0 0 0 0 0 0 piJ 0 0 --1 0 0 po 0 0 0 as@ 0 a19 0 0110 0 a,‘0 0 0 all1 0 a8l1 0 KOOOOOOOOl
a+P
a19=Gmr,
all0 =
GOfP
G
Expanding zeros)
_;
this
1
determinant it equal
0
0 dt 0 0 0
0 0 dx 0 0
0
0 1 0
0 0 0
0 0 dt 0 0’
0 00 0 0 0 dx 0
0 0 0 dt 0’
0
0
0
0
0 0 0
al00
0
i 0
a1011 0 00
0
1 +
(which
2F@)
11
p)
in not difficult
we obtain
al0
becaase
the eqnation
F’ 10=--I 'Y
al0
-WY-@)
to zero,
(2.1$
(~1
)
,f@
0
UllJ10 0
-F'W 2F@)
9--
F (~1
=911 =
,
0
--I+
G C
(~1
0
-i
0 0 1
a10
aglO =
Z,
-d+ 1 F
and setting
0
as 9=G&,
F (~1 alll =
0 0 00000 dt 0 0 dx 0 0 0 0 0 0
of the large number
for the characteristics
of of the
system
ad-{[I +k($-$-y]K
+4qG+
$G}a2+
+ ‘G + GK Ls’+ h_(~2_ $)‘“I = 0 PO(g)* = a*, It should
be noted [4] that s’,<
I-&
= 3,
1 and k < 1. When y 10,
p& equation
(2.2)
=k (2.2) redncea
to
602
A.M. Skobcav
@
(a”, s) z .’ --[(I + ks) K + 1/S (4 - 2) Gl a2 + GKs (s + k) = 0 Equation
(2.2) has been
doer, not make the problem over,
we will restrict
which
a is constant
istics
are straight In view
motion
obtained
without
K, G, and k. In the following
quantities
ourselves along
because
of the fact
solutions
to the case
equation
Since
concerning
in (1.1)
where y I 0 and will
the characteristics.
that the boundary
a’ depends
conditions
to be self-modelling.
of system
As a consequence
have
Under
of the self-modelling,
this
is nonlinear.
only consider on s alone,
the form of step assumption
all quantities
only on a, because
to depend
only on s.
From the self-modelling
we have
More-
motions
functions,
it is possible
the to const-
will
depend
all quantities
only on x/t appearing
the firat equation
(1.1) can be written au
making
use
of the third
equation
02 ap _ --__---
in (1.1)
in the form
da
(1.1).
(2.5)
we have,
respectively,
3P
at
K
= (I/$.
(2.4)
a2%=z Hence,
for
the character-
a -= at Therefore
the
assumption
(1.1).
It is clear from (2.3) that o depends can be assumed
the second
whatsoever
that G < (1 + k) K; this
assume
lines.
can be assumed
ruct some
linear,
any assumption
we will
(2.3)
(2.6)
at
(2.7) or (2.8) Integration
of (2.8) yields
VP and according
to (2.2)
= k-(po) exp (\
$
(E)
b”
we have
_
;1”+ dE) kc)
(2.9)
K
(2.10) The remaining methods.
quantities
Replacing
tions
of system
value
problems.
(1.1).
appearing
in the system
o in (2.Y) by the roots which
can be used
of equation
can be obtained
by elementary
(2.3),
a family
for the construction
we obtain of solutions
of solu-
of the boundary
elastic-plastic
Plane
Equation ones
(2.3) has
correspond
the solution
obtained
a longitudinal verse
four roots : two are positive
to waves
propagating
wave;
the larger
that obtained
and two are negative.
in the positive
by substituting
603
wavea
direction
positive
by substituting
along
root (2.3)
the smaller
The positive
the x-axis.
into (2.9)
one will
Further,
will
be called
be called
a
trans-
wave. 3. Now, let us examine
Let the larger
of a’ by assuming Solving
(2.3).
by 4
We will
and the smaller
that a* are functions
(2.3).
(1 +
?a2 =
equations
root be denoted
assnme
that (2.3)
is an eqi;ailon
one by a :. We will
obtain
in aa.
an estimate
of s.
we obtain
ks) K +
(3.1)
1/Q (4 -
s2) C h
{{(l
f
ks) K f
‘i,
(4 -
s2) cl2
-
4GKs
(s f
k).l” (3.1)
&3
=
(1 +
1/3 (4 -
ks) K +
s3) G f
{[(I
+
lis )K -
‘i, (4 -
s2) Cla +
4GKh)“’
for s < 1 h E (1 +
ks) ‘/, (4 -
3)
-
s (s +
k) L
1!3 (i -
s’) (4 +
ks) >
0
(3.la)
Therefore
a?< This
follows
(I f
=
have
Further,
a very elementary
the possible
character
(3.2a)
V(a - B)“+S2
a + B*
max(a, B)
z2 >
divide
(3.2)
from the fact that for the relation
xl,2
we always
ap2 > (1 + ks) K
k-4K,
values
analysis
shows
of the parameters
that
dal* / ds > 0
into three
cases
(3.2b) and
a,* <
in accordance
G.
with
One can the
of dd/ds.
(1). If
kK > then
daz2 I ds >
0
and
a22 > K -+ a/&
3 (If 4sk) for all values
G
(3.3)
of a.
(2). If G>kK>;G (3.4) then
a22 >
K +
‘13G and the derivative
dai/ds
changes
sign
in the interval
[0, 11.
(3). If ‘,,C
>
kK
(3.5)
604
A.M. Skobccv
then the derivative
&,a/
4. Now we will cribes will
the motion clarify
aystem
when
(1.1).
ds <
consider
K +
4/3C
1 >
o>
of system
The plasticity
condition
can be employed.
writcl (2.6)
when
of applicability
shear.
condition
we will
a,2 <
the limit
with plastic this
0,
Making
s*, where s* = LICK / 4~;.
(1.1).
System
for shear
use
will
(1.1) des-
be A > 0. We
of the third equation
in
in the form
[a2-
t
(1
-j-;)K]g = +gIzg
With the aid of (2.4) transform
and the first
the second
equation
(4*1)
equation
in (1.1)
in (l.l),
we
into
h=f($__l)$_ (4.2) =-
1/j
a% 1/l
account
where
[a% -
(C -a*)
2
has been
(s + k) K] au -
taken
tiX
s2 of (4.1).
FIG. 2 By using (4.2)
can be transformed
Thus,
if the material
=-+[a2-
is compressed,
elastically cases
(K +
then during
K + 4/3G
a2 > K f a
to show
that
(4.3)
+G)]$
loading
or unloading
the condition
respectively,
a2 <
With
it is not difficult
into the form
h
h > 0 yields,
(2.3)
wave
transverse
during
unloading
for all values
(I), (2) and (3)(s < s+) the shearing
during
anloading;
during
loading.
in case These
(au /
412G
G) the
(a 12 <
(au / 62 < 0)
shearing
differ
occurs
plastically
from the results
0)
(4.5)
plastically
of the parameters. occurs
(3)(s > s+) the shearing
results
ar >
(4.4)
during
loading
With longitudinal during
loading
during
unloading
is elastic
in [4] (p. 84) where
waves
and in
and elastically and plastic
an error has been
made. 5. Now we will ing transverse tion of (1.1). the
construct
We will
(p, p)-diagram we have
2 is the region wave.
condition
the following
ourselves
boundary
that a uniform to the case
(3.5) and the unloading
picture
of propagation
In region
of the original
and assuming
set y 3 0 and limit
ment,
the transverse
waves
satisfied
(z, I) -plane region
the solution
andlongitudinal
1 we have
: regions
value
problem
motion
is also
where branch
the loading satisfies
1, 3, and 5 are regions
of the longitudinal ~7= uu and 7=
wave,
7,, and in region
branch
in
(3.3).
In the
of uniform
move-
and region
and T- T& ; in region 3 we will set ~7= o,, and T= TV. Introducing [F (p)] Y - X, the third equation in (1.1) uniquely determines the relation
D = ol,
by combina solu-
4 that of
5 we have the notation between
u, 7 and z, 7.
Plane
Henceforth
the state
of stress
will
elastic-plastic
be described
605
waves
by the quantities
z, 7, where
we have
set
zi = [F (pi)]? If we consider see
that at first
the time variation
it is constant.
Then,
of the state
wave
to formulas
(2.9)
x0, T,, to x1, v-~. Then, I3
changed
I \
are two families
of these
to different family
of a curve
the curves
the curve fixed x on a transverse five
must
(b) in region also
lie on curve
(zl, 7,) must This
pass
means
compression
possible
cases
tom
l-4 wave,
zu7a
Hence
The
waves waves
3 has
by fixing
family been
the curve
and curve
l-3
to point
za. Let
through
by 1, and
of possible
on a longitudinal
passages compress-
in: (a) region
(1.2.3), l-3
etc.
When the solution
and, in addition, (z,,
of the problem
the curve
of the second
exists,
point
family
7J.
that
we obtain
and
and draw
passing
denoted
(zt, TJ lying
family
(aa = o:) ; the
is made
and second
first
(a’ = a:)
(za, ~a) in the (2, T) -plane
represents
correspond
curves.
a family
in Fig.
as para-
FIG. 5
through
z2 =
from
it is
in the Cz, 7) -plane.
transverse
FIG. 4
(1.3.4),
until
to zt, 7r and remains
to longitudinal
of the first
it. The point
The
changes
with aa = ai
can be regarded
There
us take the point
FIG. 3
and (2.10) of curves
choice z
(2.9)
representations
the second
etc.
of x, we
the state
constant
wave
metric
corresponds
ion wave,
passes,
value
and (2.10)
it remains
by the transverse
Formulas
with
a fixed
constant.
/
E!C-
with
as the longitudinal
according
t
of stress
z. exp Q2 (so, s2),
the equation
for sp
z1 =
z2
expml (s2,SJ
(zl, ~~1
issuing
from
606
rl.M. Skobccv
[Q>,(sr, SJ + CD2(so, sJ1 == z1
z. exp When sr = a,, the left-hand the
left-hand
curve.
side
When So + 1, the
such
that
the
Figures
4 and
considered.
other
boundary
side
5 show The
point
aide
the
than
cases
for system
side.
this is an s1
the matter.
x of z and 7on
solution
provided
above there
settles
analogously.
Their
aide,
7,) lies
Therefore
This
station
be treated (1.1).
and (zI,
to infinity.
at a fixed can
the right-hand
l-4
to the right-hand
dependence
problems
is smaller
on the curve
of (5.11 tends
is equal
remaining
value
of (5.1)
some
left-hand
left-hand
case
aide
determines
(5.1)
time
for the
It is possible
to treat in a similar
is constructed
way. Apart to treat
from the continuous
discontinuous
stability
criterion,
small
disturbances
Hence
it follows
wave
the
that
of (1.11
corresponding
velocity
ahead
if da/dp
exists
solutions
solutions
of a shock
of the wave
a compressive
wave
front shock
considered
to shock
and
must
than
exists
3, it is possible
In accordance
be greater
less
wave
in section
waves.
those
with
than
the velocities
behind
the wave
the of
front.
if do/dp > 0 and a rarefaction
shock
< 0.
We have da _=_-- 1 daa ds 2a ds dp dP From verse that
(2.7)
and
wave.
(3.2)
Now,
it will
from (5.2)
In the physically condition
(3.51,
it is clear
that
a shock
wave
wave
and
ds/dp
can
exist
only
< 0 on a transin case
(2) and
wave.
important
and the
In conclusion
ds/dp > 0 an a longitudinal
we have
be a rarefaction
(5.2)
case
unloading
the author
where
part
wishes
the
part
(3.31,
a shock
satisfies
to thank
of the (p, @-diagram
loading
N.V.
wave
Zvolinskii
cannot
for valuable
satisfies
exist. advice
and
suggestions.
BIBLIOGRAPHY 1.
Crigorian, %A., of soil
2.
dynamics1
Zvolinskii,
N.V.,
0 osnovnykh PMM,
Ob izluchenii
(Radiation of an elastic No. 1, 1960. 3.
4.
Zvollnskii, of a plastic Grigorian.
N.V., wave S.S.,
(One-dimensional
Vol.
wave
predstavleniiakh
dinamiki
gruntov
oprugoi
volny
in the
Rykov, G.V., Otrazhenie plastichaskoi from an obstacle) PMhf, Vol. 27, No.
volny 1, 1963.
quasi-static
from a spherical
pri sfaricheskom explosion
Chemous’ko,
(Basic
concepts
24, No. 6, 1960.
F.L.,
Odnomemye
motions
of soil)
vzryve ground)
PMM, Vol.
ot pregrady
kvazistaticheskie PMM, Vol.
v grunte
25, No.
dvizheniia 1, 1961.
24,
(Reflection
grunta
Plane
5.
Grigorian, (The
6.
S.S., Chernous’ko,
piston
problem
F.L.,
for the soil
Zadacha
equation)
waves
o porshna
Antsiferov, vozmnshchenii tional
in the dynamics VS.
Rakhmatulin,
of soft
disturbances
soils)
in a nonlinear
srede elastic
dlia
uravnaaii
dinamiki
gruntov
(The
Rykov, G.V., Nekotorye gruntov (Some experimental
Dokl. AN SSSR, Vol. 133, No. 6, 1960.
Kh. A., Rasprostranenie
v nelineino-uprugoi
607
PMM, Vol. 25, No. 5, 1961.
Alekseenko, V.D., Grigorian, S.S., Novgorodov, A.F., eksperimental’nye issladovaniia po dinamike miagkikh investigations
7.
elastic-plastic
szhimaiushche
propagation
medium)
sdvigainahchikh
of compressional
PUM, Vol. 28, No.3, Translated
-
dilata-
1964.
by D.B. McV.