taken
constraint
load
076
ncremental
rigid
updating
elsevier
shown
reduce
studied
1969
AFFDL
153
101
progressing
satisfying
presence
AF
elasticity
type
worked
simulated
smith
check
note
there
keeping
686
loaded
materially
appropriate
180
matter
local
certain
occur
meeting
regalbuto
varying
arising
tangential
CONCLUSIONS
reache
inter
few
reverse
initiate
even
ltd
contact
1973
should
plane
calculated
los
selected
applying
6xx
fine
uniaxial
fracture
compre
men
resulting
subsequent
inserted
mater
proposed
latter
known
PARTIAL
dattaguru
assumption
symmetry
P2
table
result
027
207
mation
solution
360
cooper
wa
set
1988
detail
zienkiewicz
pmaa
ET
deviation
need
could
interface
kukreti
per
laboratorie
behave
incr
considering
survey
application
both
1950
applicable
fn2
all
indian
ncrement
plotted
attain
peak
AE
inequality
relief
would
total
eter
development
nodal
support
181
factor
including
adopted
global
vided
portion
complete
third
fr21
progresse
mostly
2024
negative
ence
misfit
assump
during
simulating
anal
approach
chosen
modelled
isoparametric
whichever
basi
higher
rectly
poisson'
distributed
modulu
steel
relative
inverse
magnitude
geometric
7748
equation
imply
071
validate
stiffnes
sheet
attributed
post
extent
kumar
released
four
they
JZ
fairly
reversal
rig
1104
FO
linearly
experience
600
pmm
stress'
displace
entire
region
AIAA
plastic
cycle
068
SUBJECTED
joint
TR
monotonically
defor
satisfied
continuously
hill
252
near
elasto
basic
quadrilateral
pre
ANALYSIS
causing
diameter
interfacial
multi
CONTACT
bangalore
ometry
many
finite
life
extend
subject
numerical
sampath
permanent
author
lug
act
exact
every
009
model
static
national
callinan
exp
135
oad
1974
explain
identified
software
rigorou
1972
friction
benefit
fr11
possibility
presented
study
description
113
AU
case
regime
melbourne
slight
account
alone
surface
combination
slip
bauschinger
120
defined
parameter
relation
DISCUSSION
1987
beyond
MODEL
increase
017
von
OA
changing
cold
200
suggested
wherein
MN
tive
possible
implie
widely
modulii
simonen
OX
representing
realm
elli
1067
allen
law
containing
yield
specimen
qmex
introduced
accounting
achieved
uniax
sive
under
lin
regained
sequence
engng
elasti
earlier
determined
independently
raju
KJ
zone
11th
compression
face
compo
AP
angle
large
1077
ation
tural
spond
boundary
deformation
end
theory
respective
strain
nterface
long
F22
particular
without
than
force
just
initial
become
vicinity
effective
deform
monitored
earliest
department
isotropic
envelope
qxy
presentation
history
fit
consideration
tion
follow
continued
propertie
zero
concentration
harri
lead
plate
fitted
might
following
280
ially
corresponding
after
generalization
BQ
india
ghadiali
defence
FINITE
engineering
647
axy
second
difference
bound
INELASTICITY
reported
work
sponding
inser
oading
redistribution
whole
centre
three
reviewed
un2
respectively
needed
reference
min
yielding
439
pmax
mathematical
two
hardening
externally
each
compatibility
start
technique
resent
actual
it
OP2
6955
plot
624
ponent
proportional
iteration
generally
orthotropic
describe
full
progressively
changed
half
AEPI
RESULTS
limit
available
block
appl
compared
freely
one
incremen
minimum
YI
irrespec
relationship
sake
estimated
method
module
external
any
allowed
PLASTIC
material
23A
uniaxially
let
considered
detailed
most
sequentially
volved
valliappan
fract
mpa
560
january
engr
CYCLIC
happen
again
relevant
rule
still
direction
cover
phase
will
325
procedure
covering
part
540
211
iii
seen
variant
gpa
cause
refer
only
ill
prescribed
QT
problem
fatigue
structural
component
ref
convergence
OF
handle
into
good
ratio
dependent
till
alloy
then
formu
MS
max
NNP
thicknes
state
tal
algorithm
comput
de
klang
interference
harden
increasing
come
insertion
depending
1993
due
diam
400
633
introduction
1977
fixed
dimensional
reddy
linearity
1959
paper
received
NASA
uniform
calculating
mechanically
next
stresse
almost
restricted
constitutive
1995
arie
value
displacement
contain
evaluated
push
described
indicate
same
science
free
meth
proces
input
gaussian
property
termed
transition
19A
mise
optimum
some
applied
here
function
EFFECTS
REFERENCES
constant
crew
spread
respect
numbered
non
274
given
SEPARATION
analysi
hopper
T6
link
between
putation
parallel
aluminium
vector
elastic
positive
lation
though
commun
illustrated
DEFINITION
enable
ziegler
variation
axi
hyer
com
yogeswaren
les
TO
IV
doe
numer
essentially
621
taking
consider
modular
eshwar
DC
tensile
behaviour
exceeding
variou
lower
1072
ghassemieh
oversized
deflection
studie
path
using
hole
pin
since
advantage
monotonic
1996
formulated
ing
involved
other
ever
investigator
newton
oxford
university
principle
compare
literature
clearly
view
070
clearance
initiation
limited
manner
hoop
radial
within
obtained
stres
proc
dated
curve
washington
ELEMENT
partial
struct
well
progressed
recent
because
condition
bolt
configuration
subscript
level
550
pres
followed
tangent
perfectly
simulate
iter
amin
decrease
864
early
fig
equal
1955
206
vary
form
struc
smooth
used
equilibrium
figure
node
ELASTO
EP
NUMERICAL
when
SR
incremented
reached
copyright
tact
remote
re
different
unloading
moving
hence
anywhere
thu
separ
ary
further
vergence
change
METHOD
discrete
int
number
institute
enlarged
initially
now
mprovement
inelastic
step
mesh
100
300
elastically
LOADING
how
imposing
comprehensive
their
hooson
having
king
wheeler
quadrilat
unknown
included
1073
receding
7075
point
wanlin
hand
assumed
pressure
eral
carried
recede
required
flow
also
avoiding
retrace
distribution
ramamurthy
raphson
but
small
over
reaching
found
amplitude
schematic
nterference
criterion
agreement
linearitie
documented
TM
assume
boundarie
nayak
correspond
matrix
AMMRC
like
tension
subjected
ha
aerospace
JOINTS
aiet
modification
basically
advancing
take
T4
500
thesi
1200
loading
developed
extrapolation
assigned
linear
residual
transfer
depend
maintained
unit
made
field
surrounding
once
estimation
such
greater
150
degree
equivalent
current
edge
075
example
332
young'
discussed
1965
present
ARL
mech
see
analysed
pose
1069
combining
wherever
STRESS
softening
TN
maintain
ment
prager
acros
exhibit
cyclic
common
throughout
paragraph
1970
geometry
satish
diagram
comparing
gradually
maximum
iterative
prager'
EXAMPLES
afr2
interfer
five
confusion
filled
relaxation
brombolich
represent
reaction
012
out
MO
modified
element
inst
core
stage
section
consist
domain
separation
math
plasticity
side
074
bilinear
useful
15mm
updated
enough
pushing
continue
PROBLEM
use
retain
until
169
insert
increment
achievement
190
theorie
suitably
857
con
radiu
aim
rep
require
F0
aro
requirement
typical
computation
yielded
nin
corre
fastened
pointed
established
umax
1227
216
around
kinematic
cannot
along
not
constrain
amax
carrie
27t
incremental
eqn
redefined
onset
remain
circular
fastener
range
rao
effect
reduced
theta
before
checked
abstract
compressive
1323
adjoining
place
above
ojalvo
noded
viz
first
combined
structure