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New Formula for Geometric Stiffness Matrix Calculation

Abstract

The standard formula for geometric stiffness matrix calculation, which is convenient for most engineering applications, is seen to be unsatisfactory for large strains because of poor accuracy, low convergence rate, and stability. For very large compressions, the tangent stiffness in the direction of the compression can even become negative, which can be regarded as physical nonsense. So in many cases rubber materials exposed to great compression cannot be analyzed, or the analysis could lead to very poor convergence. Problems with the standard geometric stiffness matrix can even occur with a small strain in the case of plastic yielding, which eventuates even greater practical problems. The authors demonstrate that amore precisional approach would not lead to such strange and theoretically unjustified results. An improved formula that would eliminate the disadvantages mentioned above and leads to higher convergence rate and more robust computations is suggested in this paper. The new formula can be derived from the principle of virtual work using a modified Green-Lagrange strain tensor, or from equilibrium conditions where in the choice of a specific strain measure is not needed for the geometric stiffness derivation (which can also be used for derivation of geometric stiffness of a rigid truss member). The new formula has been verified in practice with many calculations and implemented in the RFEM and SCIA Engineer programs. The advantages of the new formula in comparison with the standard formula are shown using several examples.

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New Formula for Geometric Stiffness Matrix Calculation

Author: Němec, Ivan; Trcala, Miroslav; Ševčík, Ivan; Štekbauer, Hynek
Publisher: Scientific Research Publishing
Year: 2016
DOI: 10.4236//jamp.2016.44084
Source: https://dspace.vut.cz/bitstreams/85ca4d72-3825-4950-a42f-587ac47b959c/download
Jou nal o Applied Ma hema ics and Physics, 2016, 4, 733-748
Published Online Ap il 2016 in SciRes. h p://www.sci p.o g/jou nal/jamp
h p://dx.doi.o g/10.4236//jamp.2016.44084
How o ci e his pape : Němec, I., T cala, M., Še čík, I. and Š ekbaue , H. (2016) New Fo mula o Geome ic S i ness Ma-
ix Calcula ion. Jou nal o Applied Ma hema ics and Physics, 4, 733-748. h p://dx.doi.o g/10.4236//jamp.2016.44084
New Fo mula o Geome ic S i ness
Ma ix Calcula ion
I. Němec1*, M. T cala2, I. Še čík2, H. Š ekbaue 1
1Facul y o Ci il Enginee ing, B no Uni e si y o Technology, B no, Czech Republic
2FEM Consul ing, S.R.O., B no, Czech Republic
Recei ed 4 June 2015; accep ed 24 Ap il 2016; published 27 Ap il 2016
Copy igh © 2016 by au ho s and Scien i ic Resea ch Publishing Inc.
This wo k is licensed unde he C ea i e Commons A ibu ion In e na ional License (CC BY).
h p://c ea i ecommons.o g/licenses/by/4.0/
Abs ac
The s anda d o mula o geome ic s i ness ma ix calcula ion, which is con enien o mos en-
ginee ing applica ions, is seen o be unsa is ac o y o la ge s ains because o poo accu acy, low
con e gence a e, and s abili y. Fo e y la ge comp essions, he angen s i ness in he di ec ion
o he comp ession can e en become nega i e, which can be ega ded as physical nonsense. So in
many cases ubbe ma e ials exposed o g ea comp ession canno be analyzed, o he analysis
could lead o e y poo con e gence. P oblems wi h he s anda d geome ic s i ness ma ix can
e en occu wi h a small s ain in he case o plas ic yielding, which e en ua es e en g ea e p ac-
ical p oblems. The au ho s demons a e ha amo e p ecisional app oach would no lead o such
s ange and heo e ically unjus i ied esul s. An imp o ed o mula ha would elimina e he dis-
ad an ages men ioned abo e and leads o highe con e gence a e and mo e obus compu a ions
is sugges ed in his pape . The new o mula can be de i ed om he p inciple o i ual wo k us-
ing a modi ied G een-Lag ange s ain enso , o om equilib ium condi ions whe e in he choice
o a speci ic s ain measu e is no needed o he geome ic s i ness de i a ion (which can also be
used o de i a ion o geome ic s i ness o a igid uss membe ). The new o mula has been e-
i ied in p ac ice wi h many calcula ions and implemen ed in he RFEM and SCIA Enginee p o-
g ams. The ad an ages o he new o mula in compa ison wi h he s anda d o mula a e shown
using se e al examples.
Keywo ds
Geome ic S i ness, S ess S i ness, Ini ial S ess S i ness, Tangen S i ness Ma ix, Fini e
Elemen Me hod, P inciple o Vi ual Wo k, S ain Measu e
*
Co esponding au ho .
I. Němec e al.
734
1. In oduc ion
S ess s i ening is an impo an sou ce o s i ness and mus be aken in o accoun when analyzing s uc u es.
The s anda d o mula o geome ic s i ness ma ices is in oduced by a numbe o au ho s, such as Zienkie-
wicz, Ba he, Cook, Bely schko, Simo, Hughes, Bone , de Souza Ne o and o he s [1]-[10]. The s anda d o mula
has been shown o be sa is ac o y in a la ge amoun o cases, hough ce ain di icul ies such as low accu acy,
poo con e gence a e and poo solu ion s abili y we e disco e ed when sol ing p oblems ha included he
e alua ion o ex eme s ess and s ain s a es. Some au ho s, e.g. Cook [4], ha e sugges ed an imp o emen o
ba s and some au ho s deal wi h nonlinea models desc ibing la ge ( ini e) de o ma ion (s ain) beha io o ma-
e ials and s uc u es [11]-[21]. Howe e , as a as he au ho s know, no gene al solu ion o he p oblem has
been sugges ed o a 2D o 3D con inuum. Upon his asce ainmen , hough s a ose conce ning he physical es-
sence o geome ic (o s ess) s i ness and he o mula o e alua ing geome ic s i ness ma ices. As a esul , a
new o mula o geome ic s i ness ma ix calcula ion is sugges ed. The p esen a ion o his new o mula, which
should subs an ially imp o e analysis o s uc u es exposed o la ge s ain, is he subjec ma e o his pape . In
Sec ion 2, he s anda d o mula o geome ic s i ness ma ices is p esen ed. Sec ion 3 shows he physical back-
g ound o geome ic s i ness based on equilib ium. In Sec ion 4, he new, imp o ed o mula o geome ic ma-
ices is in oduced. The ad an ages o he new o mula, including a subs an ially imp o ed a e o con e gence
and s abili y, a e demons a ed by examples in Sec ion5. Conclusions a e p esen ed in Sec ion 6.
2. The S anda d Fo mula o S ess-S i ness Ma ices
Le us show he gene al calcula ion algo i hm o he geome ic s i ness ma ix (some imes also called he s ess
s i ness ma ix o ini ial s ess ma ix) o an elemen in an upda ed Lag angian o mula ion.
Le he ollowing hold o each componen
i
u
o displacemen ec o
u
:
1
n
i a ia
a
u Nu
=
=
∑
(1)
whe e
ia
u
is he alue o displacemen
i
u
in node a and n is he numbe o elemen nodes.
Le us de ine ma ix
N
as ollows:
[ ]
12
, ,,n
NN N=N II I
(2)
whe e
I
is he uni diagonal ma ix o he o de 3 × 3, whe e 3 is he dimension o he p oblem. Then, he ol-
lowing ela ion can be w i en o he displacemen ec o :
= ⋅u Nd
(3)
whe e
d
is he ec o o de o ma ion pa ame e s o he elemen con aining all he componen s
ia
u
in such an
a angemen ha o each node a all componen s
i
u
a e lis ed.
Le us de ine ma ix
a
g
con aining he i s de i a i es o base unc ions o node a wi h espec o spa ial
coo dina es
,
,
T
,
ax
a
a ay
az
N
NN
N

∂
= ⊗=

∂

I
g II
xI
(4)
and ma ix
G
, which is o med by sub-ma ices
a
g
[ ]
12
T
,,,,,
an
∂
= =
∂
N
G gg g g
x

(5)
The ope a o
⊗
deno es he enso (K onecke ) ma ix p oduc .
Fu he , le us de ine ma ix
Σ
by mul iplying each componen o he Cauchy s ess enso
σ
by he uni
diagonal ma ix:
sym.
xx xy xz
yy yz
zz
σσσ
σσ
σ


=⊗=



III
I II
I
Σ
σ
(6)
I. Němec e al.
735
I s a e o he s ess is no negligible, he po en ial ene gy o he in e nal o ces should be comple ed by he
ollowing e m:
( )
TT
TT
TT
1 11
dd
2 22
σσ
Ω
Ω
⌠

⌡
∂ ∂ ∂∂
∏ = ⊗ Ω= Ω =
∂∂
∂∂
∫u u NN
I d d dKd
xx
xx
Σ
σ
(7)
Then, he ollowing o mula o he geome ic ma ix o he elemen can be w i en:
T
T
T
dd
σ
Ω
Ω
⌠

⌡
∂∂
= Ω= Ω
∂∂
∫
NN
K GG
xx
ΣΣ
(8)
In eg a ion is ca ied ou on he de o med body
Ω
(in he cu en con igu a ion) and he de i a i es a e pe -
o med wi h espec o he spa ial coo dina es.
The componen o he ma ix
σ
K
ela ing he elemen node a o he elemen node b can also be w i en
simply in ma ix no a ion:
( )
d
ab a b
NN
σ
Ω
= ∇ ⋅∇ Ω
∫
KσI
(9)
o in indicial no a ion:
d , 1, 2, 3
ab
abij kl ij
kl
NN
K ij
xx
σ
σδ
Ω
⌠

⌡
∂∂
= Ω=
∂∂
(10)
Simila o mulae also hold o a o al Lag angian o mula ion, bu he second Piola-Ki chho s ess enso is
hen used ins ead o he Cauchy s ess, and in eg a ion is ca ied ou on he unde o med body
0
Ω
(in he o ig-
inal con igu a ion) while he de i a i es a e pe o med wi h espec o he ma e ial coo dina es.
3. The Sou ce o Geome ic S i ness—The Physical Backg ound
Le us conside he uss membe shown in Figu e 1. Node 2 is loaded by he o ce F pa allel o he x axis and
sliding in he same di ec ion. The equilib ium equa ion in he x di ec ion in node 2 can be w i en as ollows
( ) ( )
0Rx Tx F= −=
(11)
whe e
( )
cosTx N
α
=
is he ho izon al componen o he in e nal o ce a node 2 and
cos xl
α
=
.
()
Rx
is
he esidual o ou -o -balance o ce. The ho izon al s i ness
x
K
a node 2 is de ined simply by he ela ion
2
2
22
22
22
dd d d d d d
ddd d d d d
dd
1 cos sin
dd
x
xM x
R T Nx N N N l N N N x N
K xx
x x x l xl l ll x l l l l
l
Nx N x N N KK
ll l l
ll
σ
αα
     
= = = = += += − +
     
     

= + −= + =+


(12)
This o mula is independen o any s ain measu e o pe inen cons i u i e ela ions. I can be seen ha s i ness
x
K
consis s o wo pa s. The i s pa ,
xM
K
, ep esen s he ma e ial s i ness and depends on he s ain measu e
and cons i u i e ela ions. The second pa ,
x
K
σ
, which does no depend on he ma e ial o he s ain and s ess
measu es chosen, bu only on he geome y and he no mal o ce, ep esen s so-called geome ic s i ness. I can
be seen ha i he angle
α
is ze o, no geome ic s i ness will occu ega dless o he no mal o ce alue.
Le us show a de i a ion o a o mula o geome ic s i ness ma ix o a uss membe (see Figu e 2) in a ini e
elemen o mula ion and le us s a wi h a simple de i a ion based on equilib ium condi ions.
Le
d
be a ec o o he nodal displacemen s o an elemen , and le
be a ec o o esidual o ces; he
s i ness ma ix o he elemen can hen be de ined as ollows:
∂
=∂
Kd
(13)
I. Němec e al.
736
Figu e 1. T uss membe in an a bi a y posi ion in 2D.
Figu e 2. T uss membe : he x axis is he axis o he od in i s o iginal posi ion.
A geome ic (s ess) s i ness ma ix can be ob ained by an equilib ium condi ion when only he ini ial s ess
s a e and pe inen in ini esimal nodal displacemen o each ow o he ma ix is aken in o accoun . Such a de-
ini ion o a geome ic s i ness ma ix is independen o he s ain enso chosen.
To simpli y he ollowing de i a ions le ’s in oduce bo h, he coo dina es
x
wi h he
x
axis aligned wi h he
axis o he od and co esponding displacemen ec o
u
and le ’s es ic he de o ma ion o he
xy
plane.
Le he ec o o he nodal displacemen s o he elemen be
[ ]
T
11 2 2
,, ,u u =d
(14)
whe e
u
and
a e he displacemen componen s in he di ec ion o he
x
and
y
axis, espec i ely. The
well known ma e ial s i ness ma ix o he uss elemen in 2D is hen de ined by he ollowing ela ion:
1 0 10
0000
10 1 0
0000
M
EA
l
−



=
−


K
(15)
No e ha he uss elemen has no la e al ma e ial s i ness.
In gene al, a bi a y e m o a s i ness ma ix
ij
K
is de ined as he de i a i e o an unbalanced o ce
i
wi h espec o he de o ma ion pa ame e
j
d
as is de ined by (13). Based on his de ini ion, he geome ic
s i ness ma ix o he uss elemen subjec ed o ensile o ce N can be easily de i ed. The momen equilib ium
condi ion o he uss membe in he con igu a ion wi h he la e al displacemen
d
in node 1 is su icien o
ob ain he ans e sal diagonal s i ness e m
22
K
:
The momen equilib ium condi ion can be w i en as ollows:
d d cos d 0N Tl
α
−=
(16)
I. Němec e al.
737
Fo he in ini esimal angle
d
α
i can be assumed ha
cos d 1
α
=
, and he ollowing e m o he s i ness
e m
22
K
σ
can be de i ed:
22
d
d
TN
K l
σ
= =
(17)
When in oducing a displacemen
du
in he di ec ion o he axis o he membe , he end o ces a e in equi-
lib ium and no addi ional o ce and he e o e no geome ic s i ness will occu in his di ec ion.
F om equilib ium equa ions and symme y o he s i ness ma ix i is easy o de e mine he o he coe icien s
o he geome ic s i ness ma ix, pa icula ly
24
K
σ
,
42
K
σ
and
44
K
σ
. The emaining coe icien s o he ma-
ix a e ze os. The geome ic s i ness ma ix hen has he ollowing o m:
0000
010 1
0000
0 10 1
N
l
σ


−

=

−

K
(18)
The same o mula co esponds wi h Fo mula (12) and is p esen ed also by Cook in [4], he same as many
o he au ho s. The geome ic s i ness ma ix o a uss membe can also be de i ed om he p inciple o i ual
wo k, which will be desc ibed la e . Then a s ain measu e and cons i u i e law mus be in oduced, which is no
applicable o a igid uss, whe e geome ic s i ness also exis s.
The esul ing angen s i ness ma ix T
K
is de ined as he sum o he ma e ial and geome ic s i ness ma-
ix:
TM
σ
= +KK K
(19)
When applying he gene al s anda d algo i hm o geome ic s i ness ma ices o he uss elemen in ques-
ion, we ob ain:
u

= = ⋅


u Nd
(20)
[]
12 22
,NN=
N II
(21)
whe e
2
I
is he iden i y ma ix o o de 2 and he base unc ions
i
N
a e de ined as ollows:
12
1xx
NN
ll
  
= − , =
  
  
(22)
xx
∂∂
= =
∂∂
uN
d Gd
(23)
whe e
1 0 10
1
0 101
xl
−

∂
= = 
−
∂
N
G
(24)
Subs i u ing in he o mulae
x
N
A
σ
= =Σ
(25)
AlΩ= ⋅
(26)
he o mula o he geome ic s i ness ma ix eads:
TT
1 0 10
010 1
dd
10 1 0
0 10 1
x
l
N
Nl l
σ
σ
Ω
−


−

= Ω= = 
−

−

∫∫
K G G GG
(27)

I. Němec e al.
738
This geome ic s i ness ma ix di e s om ha in Fo mula (18) and in oduces also an axial s i ening. Bu
no eason was ound by he au ho s o concluding ha no mal o ce had led o a change in he axial s i ness o
he elemen . So le us de i e he geome ic s i ness ma ix o a uss elemen in a mo e undispu able way based
on he p inciple o i ual wo k.
Wi h de o ma ion es ic ed o he
xy
plane, he G een-Lag ange s ain enso is de ined
22
1
2
x xx
u u
e
x xx
εη

∂ ∂∂

=+ +=+



∂ ∂∂


(28)
whe e
22
1
,2
xx
u u
ex xx
η

∂ ∂∂

= = +



∂ ∂∂


(29)
Fo uss he p inciple o i ual wo k becomes
d
x x ex
SW
δε
Ω
Ω=
∫
(30)
whe e
x
S
is he 2nd Piola-Ki chho s ess in he
x
axes a he ollowing calcula ed ime s ep + ∆ . Assuming
equali y
x xxxxx
S SS S S
σ
+
≡ = +∆ = +∆

we ob ain he inc emen al exp ession o he (30)
dd d
x x x x ex x x
S We
δε σ δη σ δ
ΩΩ Ω
∆ Ω+ Ω= − Ω
∫∫ ∫
(31)
and he linea ized equa ion o he p inciple o i ual wo k ( i ual displacemen ) simpli ies o:
dd d
x x x x ex x x
Ee e W e
δ σδη σδ
ΩΩ Ω
Ω+ Ω= − Ω
∫∫ ∫
(32)
Assuming (25) we ob ain
xx x x
EAe el N l F u N el
δ δη δ δ
+=−
(33)
whe e
x
u
ex
δ
δ
∂
=∂
and
x
uu
xx xx
δδ
δη
∂∂ ∂∂
= +
∂∂ ∂∂
(34)
[ ]
11010
x
u
exl
∂
= = −
∂d
(35)
[ ]
TT
2
1 1 0 10
0 0000
11 1
1010
1 10 1 0
0 0000
xx
ee ll l
δδ δ
−−
  
  
  
=−=
  
−
  
  
d dd d
(36)
TT T
2
1 0 10
010 1
1
10 1 0
0 10 1
x
uu
xx xx l
δδ
δη δ δ
−


−
∂∂ ∂∂ 
=+= =

−
∂∂ ∂∂ 
−

d G Gd d d
(37)
Then he equa ion o he p inciple o i ual wo k can be w i en as ollows:
T T TT
M ex in
σ
δ δ δδ
+=−
dKd dKd d d
(38)
whe e
1 0 10 1
0000 0
,
10 1 0 1
0000 0
M in
EA N
l
−−
  
  
  
= =
  
−
  
  
K
(39)
I. Němec e al.
739
T
1 0 10
010 1
d10 1 0
0 10 1
N
l
σ
Ω
−


−

= Ω= 
−

−

∫
K GGΣ
(40)
A e ans o ma ion in o global coo dina e sys em
xx
yy
 
=
 
 
R
, whe e
( ) ( )
( ) ( )
cos sin
sin cos
CS
SC
αα
αα
 − −

= =




R
(41)
=d Td
, whe e

=

R
TR
0
0
(42)
and a e elimina ion o he ec o o i ual displacemen s we ge :
T
MM
=K TKT
(43)
22
22
22
22
M
C CS C CS
CS S CS S
EA
lC CS C CS
CS S CS S

−−

−−

=
−−

−−


K
(44)
T
1 0 10
010 1
10 1 0
0 10 1
N
l
σσ
−


−

= = 
−

−

K T KT
(45)
[ ]
T
T
in in NC SCS= =−− T
(46)
( )
M ex in
σ
+=−K Kd
(47)
The geome ic s i ness ma ix (45) is he same as ha ob ained by use he s anda d Fo mula (27) and he i s
ow o he ma ix does no co espond wi h Fo mula (12). Le us y o de i e he geome ic s i ness ma ix o a
uss elemen using a mo e accu a e s ain measu e.
The app oxima e na u e o he linea ela ion be ween he de o ma ion and displacemen can be shown on a
ib e o ini ial leng h
dS
. Wi hou any loss o gene aliza ion, le us in oduce a sys em o coo dina es
x
wi h
he o igin a he s a ing poin o he ib e and wi h he x axis o ien ed in he o iginal di ec ion o he ib e. Le us
deno e by
ds
he leng h o he ib e in he de o med body (Figu e 3).
Le us deno e by he ec o o displacemen o he s a ing poin o he ib e. The end-poin o he ib e will be
displaced by ec o
d+uu
.
Using he o mula o he body-diagonal o a cuboid wi h dimensions
ddSu+
,
d
,
dw
, we can exp ess he
new leng h o he ib e using he ollowing ela ion:
()
222
d dd d d
s Su w= + ++
(48)
In oducing s e ch
ddsS
λ
=
and conside ing
d dd d d
u w
u S Sw S
xx x
δ
∂∂ ∂
= , = , =
∂∂ ∂
(49)
we ob ain he ollowing ela ion o s e ch o he ib e:
22 2 22 2
d
1 1 12
d
x
s u w uu w
S xxx xxxx
λε
∂∂∂ ∂∂∂∂
  
=+==+++ =++++
  
∂∂∂ ∂∂∂∂
  
(50)
I. Němec e al.
740
Figu e 3. Elonga ion o ib e dS.
Le us conside he binomial heo em:
23
11
2 8 16
AA A
A+=+− + +
o
21A<
(51)
and le us ake in o accoun only he i s wo e ms. Then we can w i e:
22 2
1
12
u u w
x xxx
λ

∂ ∂∂∂

=++ + +



∂ ∂∂∂


(52)
and o
x
ε
22 2
1
12
x
u u w
x xxx
ελ

∂ ∂∂∂

= −= + + +



∂ ∂∂∂


(53)
I we wan o be mo e accu a e and ake in o accoun h ee e ms o he binomial expansion, and i we neglec
he hi d and highe powe s o he de i a i es o he displacemen componen s, we ge a mo e accu a e exp ession
o he s e ch:
22
1
12
u w
x xx
λ

∂ ∂∂
 
=++ +

 

∂ ∂∂
 

(54)
and hence
22
1
2
x
u w
x xx
ε

∂ ∂∂
 
=++

 

∂ ∂∂
 

(55)
Fo a 1D p oblem, he e o e, his mo e accu a e exp ession would be iden ical o he o mula o
x
ε
known
om linea mechanics:
x
u
x
ε
∂
=∂
(56)
Using he mo e accu a e s ain measu e we ob ain:
2
1
2
x xx
u
e
xx
εη
∂∂

=+=+

∂∂

(57)
whe e
x
u
ex
∂
=∂
,
2
1
2
x
x
η
∂

=
∂

I. Němec e al.
741
[ ]
TT T T
new new 2
0 0000
1 010 1
11 1
0 101
0 0000
1 0 10 1
x
xx l l l
δ
δη δ δ δ
  
  
−−
∂∂   
== = −=
  
∂∂   
−
  
dGGdd dd d
(58)
whe e is de ined a new ma ix
[]
new
10 101
l
= −
G
ins ead o he s anda d
G
.
The linea ized equa ion o he p inciple o i ual wo k ( i ual displacemen ) modi ies o:
T T TT
10 10 0000 1
0000 010 1 0
1010 0000 1
0000 0 101 0
ex
EA N N
ll
δ δ δδ
−−
 
 
−
 
+=−
 
−
 
−
 
d d d d d d
(59)
A e ans o ma ion in o global coo dina e sys em and elimina ion o he ec o o i ual displacemen s we ge
di e en geome ic s i ness ma ix in he o a ed and hus also in global coo dina e sys em:
T
new new
0000
010 1
d0000
0 10 1
N
l
σ
Ω


−

= Ω= 

−

∫
K GGΣ
(60)
22
22
T
22
22
S SC S SC
SC C SC C
N
lS SC S SC
SC C SC C
σσ

−−

−−

= = 
−−

−−


K T KT
(61)
Resul ing s i ness ma ix
σ
K
de i ed om he p inciple o i ual wo k, using he mo e accu a e s ain
measu e, is he same as ha de i ed om equilib ium condi ions (18) and co esponds wi h Fo mula (12).
I can be seen ha he s anda d o mula has p oduced a di e en geome ic ma ix o he 2D uss elemen
(27) han Fo mulae (18), (12) and (61) de i ed ea lie and heo e ically unjus i ied geome ic axial s i ness was
also p oduced. This o mula would lead o a poo con e gence a e, inaccu acy and e en, in he case o ex eme
comp ession, o singula i y. E.g. o
x
E
σ
= −
, ze o no mal angen s i ness would be ob ained o he uss
elemen , al hough he e is no physical eason o his. Fo
xE
σ
<−
he no mal angen s i ness would e en be
nega i e, which would be absu d. In he case o ension no s abili y p oblem would occu , bu he low con e -
gence p oblem is s ill p esen . E.g. when
xE
σ
=
, he unbalanced nodal o ces o 1/2 o he load inc emen al-
ue would occu in he i s i e a ion o he las inc emen . In he 2nd i e a ion i would be 1/4, and in he i- h i e a-
ion he unbalanced o ce o
12
i
o he load inc emen alue would s ill occu . These p oblems a e known,
and he e o e o he geome ic s i ness o uss elemen s Fo mula (18) is widely used ins ead o Fo mula (27),
which is de i ed om he gene al Fo mula (8) o (9). Then, in many compu e p og ams di e en a es o con-
e gence a e ob ained o a od modeled by a uss elemen han in he case o a uss modeled by solid ele-
men s.
To ob ain he same geome ic s i ness ma ix o he 2D uss elemen (18) as was de i ed abo e om he
equilib ium, he in luence o he membe
ux∂∂
mus be omi ed in he s anda d o mula, i.e. he i s ow o
he
G
ma ix mus be illed in wi h ze os.
4. An Imp o ed Fo mula o a Geome ic S i ness Ma ix
In oducing a ib e o cons an c oss sec ion a ea A in he di ec ion
x
o p incipal s ess in a 2D o 3D con in-
uum ins ead o a od, and assuming only nonze o s ain in he di ec ion o he ib e, and ha all he o he com-
ponen s o he s ain enso a e ze o, we can w i e a simila o mula o (12):
I. Němec e al.
748
h p://dx.doi.o g/10.1016/0045-7825(84)90062-8
[16] Cu nie , A. and Rako omanana, L. (1991) Gene alized S ain and S ess Measu es: C i ical Su ey and New Resul s.
Enginee ing T ansac ions, 39, 461-538.
[17] Chiskis, A. and Pa nes, R. (2000) Linea S ess-S ain Rela ions in Nonlinea Elas ici y. Ac a Mechanica, 146,
109-113. h p://dx.doi.o g/10.1007/BF01178798
[18] Fa ahani, K. and Naghdabadi, R. (2000) Conjuga e S esses o he Se h-Hill S ain Tenso s. In e na ional Jou nal o
Solids and S uc u es, 37, 5247-5255. h p://dx.doi.o g/10.1016/S0020-7683(99)00209-7
[19] Da ijani, H. and Naghdabadi, R. (2010) Cons i u i e Modeling o Solids a Fini ede Fo ma ion Using a Second-O de
S ess-S ain Rela ion. In e na ional Jou nal o Enginee ing Science, 48, 223-236.
h p://dx.doi.o g/10.1016/j.ijengsci.2009.08.006
[20] Hill, R. (1978) Aspec s o In a iance in Solid Mechanics. Ad ances in Applied Mechanics, 18, 1-75.
h p://dx.doi.o g/10.1016/S0065-2156(08)70264-3
[21] Fa ahani, K. and Bahai, H. (2004) Hype -Elas ic Cons i u i e Equa ions o Conjuga e S esses and S ain Tenso s o
he Se h-Hill S ain Measu es. In e na ional Jou nal o Enginee ing Science, 42, 29-41.
h p://dx.doi.o g/10.1016/S0020-7225(03)00241-6
Lis o Va iables
A
C oss sec ion a ea o a beam
C
Ma e ial angen moduli
E
Young modulus
,
M
σ
KK
Ma e ial and geome ic angen s i ness ma ix, espec i ely
,
M
σ
KK
Ma e ial and geome ic angen s i ness ma ix in p incipal axes
i
N
Shape unc ions
N
Ma ix o shape unc ions
R
Ro a ion enso
S
Second Piola-Ki chho s ess
,
in ex
WW
In e nal and ex e nal i ual wo k
d
Vec o o nodal displacemen s
ˆ
e
In ini esimal s ain
e
In ini esimal s ain in p incipalaxes
in
In e nal nodal o ces
ex
Ex e nal nodal o ces
I
Uni diagonal ma ix
l
Membe leng h
Time
u
Displacemen ield
,,u w
Displacemen s in he x, y and z di ec ions espec i ely
,,xyz
Spa ial (Eule ian) coo dina es
,,xyz
Coo dina es in p incipal aces
ε
Modi ied s ain enso in p incipalaxes
,ij
ηη
Quad a ic e ms o he modi ied s ain enso in p incipalaxes
σ
∏
Po en ial ene gy o geome ical s i ness
Σ
= ⊗ IΣ
σ
Σ
= ⊗ IΣ
σ
,ij
σσ
Cauchy s ess enso
σ
Cauchy s ess enso in p incipal axes
0
,
ΩΩ
Domain o cu en (de o med), ini ial (unde o med)