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Nonlinear Analysis of the Extreme Wind Fragility of the Reactor Hall Frame

Abstract

This paper describe the methodology and the results of the safety analysis of the Nuclear Power Plant structures under impact of the extreme climatic loads. In the case of the Nuclear Power Plant structures, the design criteria are stronger. The requirements of the international agency IAEA and NRC standards are based on the probability of mean return period equal to one per 104 years. The fragility curve of the extreme wind was determined on the base of the nonlinear probability analysis of the steel hale frame considering material and geometric nonlinearity using ANSYS software. The failure mode of the NPP structures is expressed by High Confidence of Load Probability of Failure (HCLPF).

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Nonlinear Analysis of the Extreme Wind Fragility of the Reactor Hall Frame

Author: Králik, Juraj
Publisher: Vysoká škola báňská - Technická univerzita Ostrava
Year: 2020
DOI: 10.35181/tces-2020-0004
Source: https://dspace.vsb.cz/bitstreams/56918830-ecae-4c13-9aac-9d79950a9867/download
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NONLINEAR ANALYSIS OF THE EXTREME WIND FRAGILITY
OF THE REACTOR HALL FRAME
Ju aj KRÁLIK1, Ju aj KRÁLIK, j . 2
1Depa men o S uc u al Mechanics, Facul y o Ci il Enginee ing, Slo ak Uni e si y o Technology in B a isla a,
Radlinského 11, B a isla a, Slo akia
2Academy o Fine A s and Design in B a isla a, H iezdosla o o nám. 18, B a isla a, Slo akia
ju aj.k alik@s uba.sk, [email p o ec ed]
DOI: 10.35181/ ces-2020-0004
Abs ac . This pape desc ibe he me hodology and he
esul s o he sa e y analysis o he Nuclea Powe Plan
s uc u es unde impac o he ex eme clima ic loads. In
he case o he Nuclea Powe Plan s uc u es, he design
c i e ia a e s onge . The equi emen s o he in e na ional
agency IAEA and NRC s anda ds a e based on he
p obabili y o mean e u n pe iod equal o one pe 104
yea s. The agili y cu e o he ex eme wind was
de e mined on he base o he nonlinea p obabili y
analysis o he s eel hale ame conside ing ma e ial and
geome ic nonlinea i y using ANSYS so wa e. The ailu e
mode o he NPP s uc u es is exp essed by High
Con idence o Load P obabili y o Failu e (HCLPF).
Keywo ds
NPP, Nonlinea , Sa e y, F agili y, P obabili y, Ex eme
Wind, ANSYS.
1. In oduc ion
This pape deals wi h he esis ance o he s eel hale ame
o he nuclea powe plan (NPP) wi h eac o VVER440.
These analyses a e based on he ecommenda ions o
IAEA and US NRC [1-14], expe ience om simila
analyses o NPPs ab oad [15, 16], new indings om
p obabilis ic analyses o s uc u es and own expe ience
om p e ious analyses [16]. The me hodology o
p obabilis ic analysis o NPP s uc u es a e based on he
analy ical solu ion and simula ion me hods. [17-34]. These
analyses a e based on he cu en esul s o moni o ing he
ma e ial p ope ies o he NPP s uc u es, as well as he
esul s o he analyses o he esis ance o indi idual
elemen s o he impo an s uc u es o he NPP objec s
unde he in luence o a ious ypes o ini ia ing e en s.
The in e na ional o ganiza ion IAEA in Vienna se up
he design equi emen s o he sa e y and eliabili y o he
NPP s uc u es. The ex eme en i onmen al e en s (e.g.
wind, empe a u e, snow, explosion...) a e he impo an
loads om he poin o he NPP sa e y pe o mance. The
ex eme wind loads a e de ined wi h he p obabili y o
mean e u n pe iod equal o one pe 104 yea s. This pape
deals wi h he analysis o he s eel hale ame loaded wi h
ex eme wind load. The IAEA [6-10] and NRC s anda ds
[11-13] equi e se ing up he p obabili y o he s uc u e
ailu e du ing he ex eme loads.
Fig. 1: FEM model o he NPP buildings.
Fig. 2: FEM model o he ex eme wind loads.
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The NPP wi h he eac o VVER440 consis ou buildings
– eac o building, leng hwise side building, c oss side
building and u bine hall. The FEM model (Fig. 1, 2) o
he NPP was c ea ed om ollowing elemen s in so wa e
ANSYS – BEAM188, SHELL181, SURF154 and
MASS21. The model has 996.917 elemen s wi h 444.426
nodes and 2.666.556 DOF.
Fig. 3: FEM model o he NPP u bine hale.
The c i ical s eel ame o u bine hall s uc u e was
in es iga ed (Fig. 3). The FEM model o he s eel hale
ame consis he beam and mass elemen s o ANSYS
p og am - BEAM188 and MASS21 (Fig. 4).
Fig. 4: FEM model o he c i ical s eel hale ame.
The s eel s uc u es a e made om s eel S235 wi h
ollowing nominal ma e ial p ope ies [15, 35]
y = 235MPa and u = 360MPa. (1)
The median ma e ial p ope ies a e de ined wi h
acco dance o Eu ocodes
()
ym y 12
σ
=+
and ym y
1.2
= o 0.1
σ
=, (2)
()
um u 12
σ
=+
and um u
1.2
= o 0.1
σ
=.
The IAEA sa e y s anda ds [2, 3] de ines ou
accep able le els o ailu e a e o s uc u es, sys ems and
componen s o he NPP:
A. High plas ic ailu e - la ge plas ic de o ma ion o
s uc u es, sys ems and componen s wi h p obabili y o
ailu e (collapse, c ack) equal o o g ea e han 10-1. The
in es iga ion o he s a e o he in ingemen mus be
ca ied ou by non-linea analysis.
B. Medium plas ic ailu e - la ge plas ic de o ma ion o
s uc u es, sys ems and componen s wi h p obabili y o
ailu e (collapse, c ack) om 10-2 o 10-1. The
in es iga ion o he s a e o he in ingemen mus be
ca ied ou by non-linea analysis. Accep able
equi emen s o enginee ing elemen designs a e de ined
in ASME and o AISC building s uc u es.
C. Small plas ic ailu e - limi ed plas ic de o ma ion o
s uc u es, sys ems and componen s wi h p obabili y o
ailu e (collapse, up u e) om 10-3 o 10-2. The
in es iga ion o he s uc u al sa e y is implemen ed wi h
acco dance o ASME's equi emen s.
D. Wi hou plas ic ailu e - elas ic de o ma ion o
s uc u es, sys ems and componen s wi h p obabili y o
ailu e (collapse, c ack) equal in he ange o 10-4 o 10-3
o accep able s eel s eng h c i e ia 0.8 y o 1.2 y. Fo he
p obabili y o ailu e om 10-5 o 10-4 accep able s eel
s eng h c i e ia a e less han 0.8 y.
The ex e nal e en classi ica ion, i applied, does no
imply di e en load le els o he ex e nal e en scena ios
and he e o e he design o i ems classi ied o ex e nal
e en s should e e only o he ex eme alues o design
basic ex e nal e en s, o o a combina ion o hese e en s
whe e a leas one o hem is aken a , o close o, i s
ex eme alue.
2. Loads and load combina ions
The load combina ion o he de e minis ic calcula ion was
conside ed acco ding o ENV 1990 [36] and IAEA
equi emen s [6, 7] o he ul ima e limi s a e o he
s uc u e as ollows:
• De e minis ic me hod – ex eme design si ua ion
Ed = Gd + Qd + WEd (3)
whe e Gd is he design alue o he pe manen dead loads,
Qd - he design alue o he pe manen li e loads, WEd - he
design alue o he ex eme wind load (wi h p obabili y o
ge ing highe alue o 10-4).
In he case o p obabilis ic calcula ion and he ul ima e
limi s a e o he s uc u e he load combina ion we ake
ollowing:
• P obabilis ic me hod – ex eme design si ua ion
E = G + Q + WE = g a .Gm + q a .Qm + w a .WEm (4)
whe e g a , q a , w a a e he a iable pa ame e s de ined in
he o m o he his og am calib a ed o he load
combina ion in compliance wi h Eu ocode and Gm, Qm and
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WEm a e he median alues o he pe manen dead loads,
li e loads and ex eme wind loads.
3. P obabili y nonlinea assessmen
The sa e y o he building s uc u es was de e mined by he
sa e y unc ion SF in he o m [19, 20, 25 and 30]
SF E R= and 01SF≤< (5)
whe e E is he ac ion unc ion and R is he esis ance
unc ion.
The eliabili y unc ion RF is de ined in he o m
()
,1 0RF g R E SF R E==−=−>
(6)
whe e
()
,
g
RE is he eliabili y unc ion.
The p obabili y o ailu e can be de ined by he simple
exp ession
[
]
()
0PPREPRE=<= −<

(7)
The eliabili y unc ion RF can be exp essed gene ally
as a unc ion o he s ochas ic pa ame e s X1, X2 o Xn, used
in he calcula ion o R and E.
12 n
(, ,..., )RF g X X X= (8)
The ailu e unc ion g({X}) ep esen s he condi ion
(capaci y ma gin) o he eliabili y, which can be ei he an
explici o implici unc ion o he s ochas ic pa ame e s
and can be single (de ined on one c oss-sec ion) o
complex (de ined on se e al c oss-sec ions, e.g., on a
complex ini e elemen model).
In he case o he nonlinea analysis, he co ec
solu ion o he elas ic-plas ic beha io o he s uc u es is
de e mined by he unc ion plas ici y. The HMH unc ion
o he plas ici y was used o he nonlinea solu ion o he
s eel echnology segmen s. This plas ici y unc ion is
de ined in he o m
y
R = and e
E
σ
=, (9)
whe e he e ec i e s ess (Von Mises s ess).
The ailu e o he s eel segmen s in he ame o he
PSA analysis is de ined by he limi ed alues o he
maximal s ain de o ma ion. This ailu e unc ion is
de ined in he o m
ay,θ
R
ε
= and e
E
ε
=, (10)
whe e he e ec i e s ain (Von Mises s ain).
The ailu e p obabili y is calcula ed om he
e alua ion o he s a is ical pa ame e s and heo e ical
model o he p obabili y dis ibu ion o he eliabili y
unc ion Z = g(X) using he simula ion me hods. The
ailu e p obabili y is de ined as he bes es ima ion on he
base o nume ical simula ions in he o m
()
1
10
N
i
i
PIgX
N=
=≤


 (11)
whe e N in he numbe o simula ions, g(.) is he ailu e
unc ion, I[.] is he unc ion wi h alue 1, i he condi ion
in he squa e b acke is ul illed, o he wise is equal 0.
4. Wind load
The load on a s uc u e due o he wind is depended on bo h
wind eloci y and e ain oughness [37, 38]. The wind
eloci y and he eloci y p essu e a e composed o a mean
and a luc ua ing componen . The mean wind eloci y m
should be de e mined om he basic wind eloci y b
which depends on he wind clima e and he heigh
a ia ion o he wind de e mined om he e ain
oughness and o og aphy. The luc ua ing componen o
he wind is ep esen ed by he u bulence in ensi y.
Acco ding o STN EN 1991-1-4 [37] e ain
co esponds o e ain ca ego y I, wi h he basic wind
eloci y b.o = 24 m/s, which co espond o basic wind
p essu e qb = 0,36 kNm-2 .
The basic wind eloci y should be calcula ed acco ding
o [37] as:
b = cdi .cseason. b,0 = 1.1.24 = 24 m/s (12)
whe e b is he basic wind eloci y, de ined as a unc ion
o wind di ec ion and ime o yea a 10 m abo e g ound
o e ain ca ego y I, b,0 is he undamen al alue o he
basic wind eloci y, cdi is he di ec ional ac o , cseason is
he season ac o .
The oughness ac o c (z) accoun s o he a iabili y
o he mean wind eloci y a he si e o he s uc u e due o
he heigh abo e g ound le el and he g ound oughness o
he e ain upwind o he s uc u e in he wind di ec ion
conside ed and should be calcula ed acco ding o [37] as:
c (z) = k .ln(z/z0) = 0.19.ln(30.85/0.05) = 1.007 (13)
whe e z0 is he oughness leng h, k e ain ac o
depending on he oughness leng h z0 calcula ed using
k = 0.19(z0/z0,II)0.07 = 0.19(0.05/0.05)0.07 = 0.19 (14)
whe e z0,II = 0.05m ( e ain ca ego y II), zmin is he
minimum heigh , zmax is o be aken as 200m, unless
o he wise speci ied in he NA, z0, zmin depend on he e ain
ca ego y. Recommended alues a e gi en in [37]
depending on i e ep esen a i e e ain ca ego ies. Whe e
o og aphy (e.g. hills, cli s e c.) inc eases wind eloci ies
by mo e han 5% he e ec s should be conside ed using
he o og aphy ac o c0.
The mean wind eloci y m(z) a a heigh z abo e he
e ain depends on he e ain oughness and o og aphy
and on he basic wind eloci y, b, and should be calcula ed
acco ding o STN ENV 1991 [37] as:
m(z) = c (z).c0(z), b = 1.007.1.24 = 24.16 m/s (15)
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whe e c (z) is he oughness ac o , c0(z) is he o og aphy
ac o , aken as 1.0 unless o he wise speci ied. The
in luence o neighbo ing s uc u es on he wind eloci y
should be conside ed acco ding o STN ENV 1991 [37].
Ex e nal p essu e coe icien s o duo pi ch oo s we e
aken acco ding o STN ENV 1991 [37] o examined
ame, wi h his loca ion in middle o he hall, wi h angel
o oo ≤ 5° o di e en wind di ec ions. The ne p essu e
on a oo on he opposi e su aces was aken as a posi i e
and di ec ed owa ds he su ace, p essu e coe icien o
he in e nal p essu e cpi = + 0.2.
The ex eme wind load (EWL) was de e mined om
he maximum wind speed de e mined om he SHMU
measu emen s [39] in he NPP locali y o he e u n pe iod
10-4 by yea and he p obabili y o non-exceedance 95%
ewl.b = 53.9 m/s and p essu e pewl.b = 1.816kPa (16)
The p essu e om he ex eme wind load is 4.98x
highe han he design basic alue.
To ex apola e he maximum quan i y o ain all om
me eo ological measu emen esul s on he quan i y o
ain all (measu ed in he ime pe iod om 12 o 48 hou s),
o a mean ime o ecu ence 102 o 104 yea s, i is
ecommended o use he Gumbel p obabili y dis ibu ion
wi h he equi emen ha he p obabili y o he excess
quan i y o ain all wi h mean ime epea 102, espec i ely
104 yea s, du ing he design o he powe plan li e ime is
less han 0.5, espec i ely 0.005.
The mean alues o he ex eme wind eloci y and
wind p essu e a e ollowing
ewl.m = 47.6 m/s and p essu e pewl.m = 1.437kPa (17)
5. Load Failu e E ec
The ailu e e ec o he ex eme load on he yield s eng h
py is de e mined o he selec ed c i ical elemen s o he
s uc u e, elying on he esul s o de e minis ic analyses
o he design alues o he load and s uc u al esis ance
e ec s and he ailu e condi ion o he gi en s ess case.
In he case o p obabilis ic analysis, he mean alues o he
inpu a iables, he median alues o he s a ic o ces om
he e ec s o he load Em and he co esponding esis ance
alue o he s uc u e Rm. I we conside he load
combina ion acco ding o he ela ions (1) and he s a ic
quan i y om he e ec o he ex eme load Eewl o sepa a e
om he o he e ec s o he o he load Eo, hen he ailu e
e ec o he load py ge s in he ollowing o m
yyewl
.
p
p
η
=, (18)
whe e he pa ame e ηy is de ined om he eliabili y
unc ion RF (Eq.4 and 8).
Fo he es ima ion o he ailu e (collapse o a pa o
he s uc u e o he whole) i is also possible o use he
philosophy o de e mina ion o he limi s a e by he
pa ame e HCLPF (High con idence o low p obabili y o
ailu e) [11, 15], which is used mainly o e alua ion o
seismic esis ance o he s uc u e. Hence, HCLPF is
de e mined by he lowes esis ance o an elemen o a
gi en s uc u e as a whole and exp esses he ela i e
esis ance o he elemen o a speci ied ex eme load
exp essed by he ex eme load ailu e p essu e. This
me hodology gi es a good "es ima e" o he s uc u al
esis ance, bu does no accu a ely e lec he ma gin o
esis ance o he elemen s o he combined s ess cases
because s eng h condi ions a e non-linea in na u e.
The pa ame e HCLPF is de e mined om he
ela ionship
HCLPF (CDFM) = kD. Py = kD.
η
y.Pewl, (19)
whe e kD is he duc ili y ac o exp essing he capaci y o
a s uc u al membe o sys em.
6. Fo mula ion o F agili y Cu es
The p obabili y a ing is based on limi s a es. Limi s a es
a e possible ypes o aul s in NPP objec unc ions. The
he me ic zone is in e p e ed as an eme ging leak, which
can be a small con olled leak o a la ge ca as ophic c ack
o b eakage. The median load-bea ing capaci y o a gi en
ype o diso de depends la gely on se e al ac o s,
including ma e ial p ope ies, model assump ions, and
ailu e c i e ia. These ac o s a e cha ac e ized by
unce ain y and a iabili y, which mus be aken in o
accoun in he p obabili y e alua ion o he p essu e
iola ion. The p essu e ca ying capaci y o each ype o
diso de is exp essed as a andom a iable wi h logno mal
dis ibu ion when he unce ain y/ a iabili y is
inco po a ed in o he o mula ion (by de ini ion, he
andom a iable is logno mal di ided i i s na u al
loga i hm is no mally dis ibu ed).
In case o using analy ical me hods and FORM me hod
o ailu e p obabili y e alua ion, p essu e esis ance can
be exp essed only om wo pa ame e s - model and
ma e ial unce ain y. The ailu e esis ance is desc ibed as:
pu = pm.e a a (20)
whe e pm is he median o he ailu e capaci y, e a is he
loga i hmically dis ibu ed andom a iable wi h he uni
median and loga i hmic s anda d de ia ion βE (i.e., Em =
1.0 and βE2 = Va [ln(E)], whe e ln(E) is he na u al
loga i hm a is a logno mal dis ibu ion o a andom
a iable wi h a uni a y median alue and a loga i hmic
s anda d de ia ion o βR (i.e. Rm = 1.0 and βR2 = Va
[ln(R)]), ep esen ing he unce ain y o ma e ial
p ope ies.
Using he na u al loga i hm o equa ion (20) we ge :
ln(pu) = ln(pm) + ln(e a ) + ln( a ) (21)
The i s exp ession on he igh is a cons an
(de e minis ic) numbe , while he second and hi d
exp essions a e no mally dis ibu ed andom a iables.
Acco ding o he basic heo y o p obabili y, he sum o
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no mally dis ibu ed independen andom a iables is
no mally di ided, wi h βC2 sca e ing equal o he sum o
he de ia ions o andom a iable elemen s, i.e. in his
case:
βC2 = (βE2 + βR2) (22)
Based on he assump ion ha andom modelling
a iables and andom a iables o ma e ial p ope ies a e
independen , βC can be conside ed as a "composi e"
loga i hmic s anda d de ia ion.
Thus, he ailu e capaci y o each ype o diso de is
de ined in e ms o h ee pa ame e s: he median ailu e
a e Pm, he loga i hmic s anda d de ia ion βE
(co esponding o he andom a iable unce ain y o he
load e ec E) and he loga i hmic s anda d de ia ion βR
(co esponding o he andom a iable unce ain y o he
s uc u al esis ance R). Sca e ing is due o a lack o
knowledge o he di e ences be ween he analy ical model
and he eal design as well as ma e ial p ope ies. Model
inde e minacy is in luenced by simpli ying assump ions,
model de ails, and hei abili y o cap u e gli ch condi ions
on he ac ual s uc u e (also design e sus ac ual
de ia ion). The unce ain y o he s eng h o he ma e ial
lies in he lack o in o ma ion on i s p ope ies as well as
hei a iabili y. Examples o sou ces o such unce ain ies
include: a iabili y in conc e e s eng h, s eel slip limi ,
s ess-s ain ela ionship, s eel shell s eng h, and
empe a u e in luence on ma e ial s eng h. I expe i-
men al da a on ac ual ma e ial s eng h p ope ies a e
a ailable, hey can be used o es ima e βR.
In p ac ice, howe e , he de e mina ion o he βE and
βR pa ame e s is la gely a ma e o good enginee ing
es ima ion. In de e mining he ealis ic alues o β,
expe ience om p e ious p obabilis ic s uc u al analyses,
e.g. o e p essu e s udies, seismic isk p obabili y
assessmen s, e c. and expe ience in de e mining he load-
bea ing capaci y o a ious elemen s by es and analy ical
me hods. F om a p ac ical poin o iew, he p obabili y o
a alue o less han 90% is less han 5% when using a
pa icula model / o mula. In his case
βE = - ln (0.9) / 1.65 = 0.06 (23)
The ac o 1.65 is due o he ac ha he alue o a
no mally dis ibu ed andom a iable ha is exceeded wi h
a p obabili y o 95% is he mean educed by 1.65 imes he
s anda d de ia ion. I he gi en alue is exceeded wi h
84% p obabili y, exp (-0.006) = 0.94, i is 94% o he bes
es ima e alue.
The p obabili y o ailu e occu ing a a p essu e less
han a speci ic alue o in e nal p essu e, pu, is exp essed
in he case o logno mal dis ibu ion as
()()
ewlu um
P ob ln C
ppp pp
Φ
β
=≤=

(24)
whe e p is p obabili y ailu e occu s a a p essu e less han
o equal o pu, pewl is a andom p essu e capaci y,
Φ
(.) is a
cumula i e dis ibu ion unc ion o a s anda d no mal
andom a iable, ln(.) is a na u al loga i hm, pm is a median
p essu e capaci y,
β
C is a loga i hmic s anda d de ia ion o
p.
The i s s ep o a wind p essu e e alua ion is he
iden i ica ion o po en ial ailu e modes. Once he
po en ial ailu e modes a e iden i ied, ailu e c i e ia a e o
be es ablished om which he median capaci ies a e
es ima ed. Fo each ailu e mode, he median capaci ies a e
o be e alua ed by conduc ing independen limi s a e
analyses using he speci ic ailu e c i e ia wi h he applied
loading consis ing o wind p essu e and dead load. Along
wi h he p essu e capaci ies o he leak ype ailu e modes,
leak a eas a e o be es ima ed in a p obabilis ic manne .
The expec ed leak a eas a e ailu e mode dependen . A e
calcula ion o he agili y o condi ional p obabili y o
ailu e o s uc u e a di e en loca ions we mus o
conside a combina ion o wind p essu e induced ailu e
p obabili ies o di e en b eak o leak loca ions wi hin
building.
Fig. 5: Family o F agili y Cu es Showing Modeling Unce ain y
Tu bine hall may ail a di e en loca ions unde
di e en ailu e modes (Fig. 5). Conside wo ailu e
modes A and B, each wi h n - agili y cu es and
espec i e p obabili ies pi (i=1,…,n) and qj (j=1,…,n).
Then he union C = A∪B, he agili y FCij(x) is gi en by
𝐹󰇛𝑥󰇜=𝐹󰇛𝑥󰇜+𝐹󰇛𝑥󰇜−𝐹
󰇛𝑥󰇜∩𝐹
󰇛𝑥󰇜 (25)
whe e he subsc ip s i and j indica e one o n - agili y
cu es o he ailu e modes and x deno e a speci ic alue
o he p essu e wi hin he con ainmen . The p obabili y pij
associa ed wi h agili y cu e FCij(x) is gi en by pi. qj i
he median capaci ies o he ailu e modes a e independen .
The esul o he in e sec ion e m in (22) is FAj(x) .FBj(x)
when he andomness in he ailu e mode capaci ies is
independen and min[FAi(x), FBj(x)] when he ailu e
modes a e pe ec ly dependen .
The low is and he consequence o an acciden
depends on he o al leak a ea. Mul iple leaks a di e en
loca ions o he con ainmen (e.g. bellows, ha ch, and
ai lock) may con ibu e o he o al leak a ea. Using he
me hodology desc ibed abo e, we can ob ain he agili y
cu es o leak a each loca ion.
Fo a gi en acciden sequence, he induced acciden
p essu e p obabili y dis ibu ion, h(x), is known. This is
con ol ed wi h he agili y cu e o each leak loca ion o
ob ain he p obabili y o leak om ha loca ion (PLi). I is
unde s ood ha he e is no b eak o con ainmen up u e a
his p essu e.

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𝑝 =ℎ󰇛𝑥󰇜󰇟1−𝐹
󰇛𝑥󰇜󰇠𝐹󰇛𝑥󰇜𝑑𝑥

, (26)
He e he Fb(x) is he agili y o b eak a he loca ion
and Fl(x) is he agili y o leak. The leak is o each
loca ion is only speci ied as a andom a iable wi h a
p obabili y dis ibu ion. This dis ibu ion o leak a ea is
disc edi ed in o a numbe o anges wi h associa ed
p obabili ies (aij, Pij). The e o e, he p obabili y o aij
occu ing (i.e. loca ion i and a e ange j) is PLi*Pij . This is
accomplished using he DPD logic. Al e na i ely, a Mon e
Ca lo simula ion could be done by andomly sampling
om each leak a e dis ibu ion ( om di e en loca ions)
and summing hem.
I we use simula ion me hods based on Mon e Ca lo o
LHS me hodology, se e al ac o s a ec ing he ailu e o
he s uc u al elemen can be aken in o accoun in he
calcula ion o he ailu e p obabili y. Abo e all, i is a ac
ha o he e ec s also condi ion he s uc u al elemen
capaci y. The design o he NPP can be b oken a di e en
loca ions, wi h di e en ypes o ex eme loads. I each
ype o ailu e leads o a collapse o he building s uc u e
o same p incipal s uc u al sys em, i is no necessa y o
check mul iple ypes o ailu e. I he consequences o he
ypes o ailu es a e he same, hen he p obabili y o
ailu e could be calcula ed as he p obabili y o a "g oup"
o se e al ypes o ailu es.
7. Nonlinea analysis
The 2D model o he c i ical ame o he u bine hall
s uc u es was c ea ed om a spa ial model by selec ing
using he subs uc u e me hod [15]. The s i ness and
weigh o he elemen s as well as he load co espond o
he alues in he spa ial model. The model con ains 660
elemen s and 1074 nodes (Fig. 6). The model was es ed
by linea calcula ion om i s own g a i y and shows he
same maximum de lec ion alues. The limi s a e o he
s eel ame was conside ed o u ilize he geome ic and
ma e ial nonlinea i y in p og am ANSYS [15]. The
geome ic nonlinea i y is based on he heo y o he la ge
s ain, which is o en used o elas ic-plas ic elemen s. The
elas ic-plas ic model o s eel ma e ial was aken in
compliance wi h he Von Mises yield unc ion [39-42]. The
New on-Raphson i e a ion me hod o sol e nonlinea
equa ions was conside ed.
The plas ici y model is de ined as shown on Fig. 7, as
mul ilinea iso opic ha dening ma e ial model.
The nonlinea analysis based on po en ial heo y
conside ing he iso opic ma e ial p ope ies was made o
he beam elemen s BEAM188 in he FEM model. The s eel
is ypical iso opic ma e ial. The elas ic-plas ic beha io o
he iso opic ma e ials is desc ibed by he Hube -Mises-
Hencky (HMH) yield c i e ion.
Fig. 6: Model o ex eme wind loads.
Fig. 7: Elas o-plas ic S ess-S ain Cu e.
Consequen ly he s ess-s ain ela ions a e ob ained
om he ollowing ela ions
{}
[]
{}
{}
()
[]
{}
pl
el el
σεε ελ
σ
∂

=−=−


∂


Q
dDdd Ddd
o
{
}
{
}
ep
σε

=
dDd
(27)
whe e ep


D is elas ic-plas ic ma ix in he o m
[]
[] []
[]
ee
ep e
e
T
T
QF
DD
DD
F
Q
AD
∂∂
∂σ ∂σ
∂∂
∂σ ∂σ




=−
  
+ 
 
(28)
The ha dening pa ame e A depends on he yield
unc ion and model o ha dening (iso opic o kinema ic).
HMH yield c i e ion is de ined in he o m
()
eq T
σσκ
= , (29)
whe e eq
σ
is equi alen s ess in he poin and
()
T
σκ
is
he yield s ess depends on he ha dening.
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Tab.1: Calcula ion o HCLPF pa ame e om nonlinea analysis on 2D
ame o he u bine hall
Limi Pa am. Loads HCLPF [kPa]
s a e
η
inc emen 50% 95%
y 4 0,35 2,542 1,828
u 4 0,62 4,576 3,290
The nonlinea analyze o he c i ical ames o NPP
u bine hall objec s was pe o med by he New on-
Raphson me hod in 74 i e a ion s eps o he 63 loads
inc emen s. The o al load was conside ed o be a mul iple
o he design load om ex eme wind o
η
= 4.
Fig. 8: De o ma ion o he ame o he HCLPF=4.576 kPa.
Fig. 9: Equi alen s ess o he ame o he HCLPF=4.576 kPa.
The ailu e capaci y o ame on ex eme wind load is
ob ained om plas ic calcula ion o ame [15]. The
agili y cu e o he ex eme wind was calcula ed on he
base o he nonlinea de e minis ic analysis o he s eel
ame o median alues o inpu da a. The p obabili y o
he s uc u e ailu e was calcula ed o he a ious le els
o he wind loads. On he base o he nonlinea
de e minis ic analysis he ac o o ailu e was calcula ed
on he s eel hall ame. The Figs. 8-10 show esul s o 4x
highe alue o he ex eme wind load. On base o he
nonlinea de e minis ic calcula ion we ha e he median
alue o he maximum wind load o elas ic limi e s a e ( y)
and plas ic limi s a e ( u) (Tab.1) as ollows
py.m = 2.542kPa and pu.m = 4.576kPa (30)
Fig. 10: Maximal capaci y o ex eme wind.
The duc ili y ac o can be de e mined as he a io
be ween he plas ic limi load and elas ic limi s a e
Duy
2.48/1.40 1.77k
η
η
== =
(31)
8. Unce ain ies o inpu da a
The unce ain ies o he inpu da a – ac ion e ec and
esis ance a e o he case o he p obabilis ic calcula ion
o he s uc u e eliabili y de ined in JCSS [44] and
Eu ocode 1990 [36].
Tab.2: P obabilis ic model o inpu pa ame e s.
Name Quan i y Cha ac .
Value
Va iable
Pa ame .
His og am
Ma e ial Young’s Modulus E
k
e
a
No mal
Load Dead G
k
g
a
No mal
Li e Q
k
q
a
Gumbel
Ex eme Wind W
k
w
a
Gumbel
Resis ance S eel S eng h
sk
F
k
a
Logno mal
Model Ac ion Unce ain M
E
m
e. a
No mal
Resis ance Unce . M
R
m
. a
No mal
Tab.3: Cha ac e is ic inpu da a o he p obabilis ic model.
Name Quan i y Mean S and.
De ia i
on
Min.
Value
Max.
Value
Ma e ial Young’s Modulus 1 0.120 0.645 1.293
Load Dead 1 0.010 0.755 1.282
Li e 0.60 0.200 0 1
Ex eme Wind 0.30 0.150 0.500 1.032
Resis ance S eel S eng h
sk
1 0.100 0.726 1.325
Model Ac ion Unce ain 1 0.100 0.875 1.135
Resis ance Unce . 1 0.100 0.875 1.135
The s i ness o he s uc u e is de e mined wi h he
median alue o Young’s modulus Em and a iable ac o
e a . Loads a e ep esen ed by hei s cha ac e is ic alues
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Gm, Qm, WE,m and a iable ac o s g a , q a and w a . The
esis ance o he s eel is delimi ed by he cha ac e is ic
alues o he s eng h ak and he a iable ac o a . The
unce ain ies o he calcula ion model a e conside ed by
a iable model ac o and a iable load ac o o Gauss‘s
no mal dis ibu ion.
The eliabili y analyses o he s uc u es a e
di e en ia ed om he poin o iew o design quan i ies
as he nonlinea de e minis ic analyses [24]. In s ochas ic
analysis, he mean alues and he s anda d de ia ion o he
a iable quan i ies a e calcula ed analy ically o
nume ically using Mon e Ca lo simula ion, which gi es us
he mo e accu a e esul s han de e minis ic alues.
Sensi i i y analysis calcula es he dominan impac o he
ou pu quan i ies and he p obabili y o he ailu e is
de ined in compa ison wi h he simula ed quan i ies in
p obabilis ic analysis.
9. Wind agili y cu e o ame
The p obabili y o he s eel ame ailu e was de e mined
by he p obabilis ic analysis based on nonlinea analysis
using he analy ical and simula ion me hods. The agili y
cu e was calcula ed o a ious le els o wind loads using
he esul s om he nonlinea analysis o he s eel hall
ame.
The p obabili y o ame ailu e was de e mined by wo
me hods:
A. Analy ical analysis based on he FORM me hod and
conside ing he logno mal dis ibu ion o ac ion e ec E
and esis ance R,
B. LHS simula ion me hods in so wa e FREeT [31],
conside ing he dis ibu ion o Gumbel's wind load, no mal
sel -weigh dis ibu ion, and logno mal o esis ance (see
Tab. 2-3).
A) FORM es ima ion o ailu e p obabili y:
We conside he median alue o he load limi e ec
pwm = 4.576 MPa acco ding o Tab. 1, he loga i hmic
s anda d de ia ion o load a e conside ed by alues
β
E =
0.1 and esis ance
β
R = 0.1. We ha e ollowing
22
CER
0.141
βββ
=+= and (32)
EWLN.95 wm C
exp( 1.65 ) 3.133HCLPF p
β
=−=
kPa
In he case o ex eme wind loads, i is an ex eme load in
he ange o 10 min. impac on s uc u e. In his case i is
possible o conside he plas ic ese e o he uss gi de ,
o beam espec i ely. In he case o he simple console o
beam simply suppo ed he duc ili y ac o is equi alen o
kD = 1.5. Then we ge he alue o he limi load capaci y
calcula ed om he linea analysis conside ing he
duc ili y ac o
EWLD.95 D wm C
exp( 1.65 ) 1.836HCLPF k p kPa
β
=−=
(33)
B) LHS simula ion using he so wa e FREeT [31]
The calcula ion based on LHS simula ion me hod (Figs.
11-13) is based on he No mal load dis ibu ion o he sel -
weigh , he dis ibu ion o he ex eme wind load in he
o m o a Gumbel dis ibu ion, and he Logno mal
dis ibu ion o he s uc u al esis ance. The HCLPF
pa ame e de e mined by he p obabili y analysis o he
u bine hall ame unde ex eme wind load by LHS
simula ion me hod o 1000 simula ions was ob ained as
ollows
()
EWLD.95 1.8191HCLPF LHS kPa= (34)
The wind agili y cu e o he s eel hall ame is p esen ed
in Fig. 13. This cu e was calcula ed by LHS me hod using
he p og am FREET.
Fig. 11: His og am o he ex eme wind load.
Fig. 12: His og am o HCLPF pa ame e o ex eme wind load.
Fig. 13: Wind agili y cu e o he s eel hall ame.
10. Conclusion
This pape p esen s he eliabili y analysis o he s eel hall
ame esis ance due o ex eme wind loads [30]. The
ex eme loads we e de ined o mean e u n pe iod equal
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o one pe 104 yea s in acco dance o he IAEA
equi emen s o NPP s uc u es [5 o 10]. The geome ic
and ma e ial nonlinea i y we e aken in o accoun . The
de e minis ic and p obabilis ic analysis o he s uc u e
ailu e was in es iga ed. The limi s a e ( ame collapse)
was ob ained om de e minis ic analysis o he ac o
ηu=2.48. The p obabili y o ailu e was calcula ed on
p og am FREET using LHS me hod [31]. The p obabili y
o ailu e alue is lowe han 10-6. In he case o he wind
load mul iplied by ac o ηu = 2.48 he p obabili y o ailu e
is equal o 0.0087. The wind agili y cu e o he s eel hall
ame was de e mined using LHS me hod o a ious le el
o he wind load.
The lowes ailu e load alues (HCLPF) assuming a
95% p obabili y o no exceeding he ul ima e limi
c i e ion on NPP s uc u al elemen s based on linea
analysis a e as ollows:
• Ex eme wind: HCLPFEWL.95 = 1.224 kPa
Conside ing he minimum duc ili y alue o kD = 1.5 based
on he assump ion o he plas ic ese e co esponding o
he s a ic unce ain y o he ame sys ems, wi h he sho -
e m exposu e o ex eme loads, we ha e he ollowing
alues:
• Ex eme wind: HCLPFEWLD.95 = 1.819 kPa
Lowes Failu e Loads (HCLPF) assuming 95% p obabili y
o no exceeding he s uc u al ailu e c i e ion o c i ical
ames wi h duo-pi ch P a T uss and beam based on
nonlinea analysis a e as ollows:
• Ex eme wind: HCLPFEWLN.95 = 3.133 kPa
The esul s o his analysis clea ly con i m ha u bine hall
s uc u es ha e signi ican ly g ea e esis ance o ex eme
snow and ex eme wind e ec s a he o igin o and he
de elopmen o plas ic de o ma ions, conside ing he
conse a i e linea calcula ion and assessmen o one
(weakes ) c oss-sec ion o he c i ical elemen .
Acknowledgemen
This p ojec was pe o med wi h he inancial suppo o
he G an Agency SR (VEGA 1/0265/16).
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