Notes and Thing to be considered:
Axial load is positve compression and negatve ension Spreadshee Spreadshee is able able o calcula calculae e all kind of of I-secton I-secton - as a mae maerr of fac fac i is prepared prepared o o be memdes memdes sow sow All calculatons are based on &'S(")$) chaper #*+*,* and .ac .a ch h he he fac faco orr k k /wi /wis s res resra rain in sinc since e i need needss o o be be calc calcul ula aed ed usi using ng val value ue fro from m ab able le #0+ #0+0" 0"/1 /120 20 3his 3his spr spr .e need o deermine deermine he value of 6m depending on he siuaton or we can provide he bending bending momen 4m value will be used in some alernatve design provision formulae for combined actons - 5ll his value if
are supplemenary since memdes can model assymmeric beam and fy ! "#$ %pa beam adshee won calculae hem (2 value value a 7uarer 7uarer poins poins of a segmen0 segmen0 8lease 8lease read commena commenary ry chaper chaper # of &'S(")$) &'S(")$) as i provides provides 6m v we wan more economical resuls - leave i blank oherwise0
are supplemenary since memdes can model assymmeric beam and fy ! "#$ %pa beam adshee won calculae hem (2 value value a 7uarer 7uarer poins poins of a segmen0 segmen0 8lease 8lease read commena commenary ry chaper chaper # of &'S(")$) &'S(")$) as i provides provides 6m v we wan more economical resuls - leave i blank oherwise0
alue for some common cases
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!a# "CR
$
%&''
H xx
!
+1+$
mm
fyf
!
"#$
m8a
%Gx !
#$$
k& m
H yy
!
+1+$
mm
fyw
!
"#$
m8a
%Gy !
1#$
k& m
H
!
+1+$
mm
fu
!
)#$
m8a
BG !
$$
k&
<
!
@$#$$$ m8a
ompressed ange %Gm !
#$$
k& m
k
!
101@
%G@ !
1@#
k& m
kl
!
1
%G" !
@#$
k& m
kr
!
1
%G) ! 6m !
",# 10@
k& m
ke 6m
!
1
d !
"#$
mm
A
!
#@##$
mm@
cx
!
$
mm
b !
)$$
mm
x
!
@$$0#
mm
cy
!
$01)
mm
bb !
)$1
mm
y
!
1,)0+ mm
Iw
!
10@
!
#$
mm
Ixx
!
K0,#
Sx
!
+0,K
b !
#$
mm
Iyy
!
#0"
Sy
!
)01,
w !
#$
mm
9
!
)0"
'x
!
#0#+
rx
!
1"+01
'y
!
@0+
ry
!
1$101
!
!
3:8
4m-x
!
$
4m-y
!
$
Ghis will overwrie he value on he le
)& SECTION *RO*ERTIES
3ype !
.;
'& (EN"IN+ AN" SEAR CA*ACITY - N,S'. C&/ Major x-axis slenderness parameter
3op Clange slenderness parameer Ls Le ! b ? G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /)$$ - #$2 ? @ ? #$ G s7r /"#$ ? @#$2 ! )01) Ley ! 1)
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $0@K+ ;oom Clange slenderness parameer Ls Le ! bb ? b G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /)$1 - #$2 ? @ ? #$ G s7r /"#$ ? @#$2 ! )01# Ley ! 1)
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $0@K+ .eb slenderness parameer Ls Le ! dw ? w G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /"#$ - #$ - #$2 ? #$ G s7r /"#$ ? @#$2 ! #0K@ Ley ! 1"$
file:///conversion/tmp/scratch/362140164.xlsx
for unsymmerical secton := weak axis bending exiss
)
Le ? Ley ! $0$)+ 9:; &A%<
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!a# "CR
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ritcal slenderness - maMor x-axis %ax Le ? Ley ! $0@K+
---N
boh ange critcal
---N
Sec0on is co12act
Ls secton ! )01) Lsp ! Lsy ! 1) 31a4or #-a#is5
secton in x-axis mm)
NZS:3404 - 5.2.2.3 - 5.2.2.5
Le ! b ? G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
'ex ! +0,K
3op Clange slenderness parameer Ls ! /)$$ - #$2 ? @ ? #$ G s7r /"#$ ? @#$2 ! )01) Ley ! @@
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $01 ;oom Clange slenderness parameer Ls Le ! bb ? b G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /)$1 - #$2 ? @ ? #$ G s7r /"#$ ? @#$2 ! )01# Ley ! @@
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $01K .eb slenderness parameer Ls Le ! dw ? w G s7r /fyw ? @#$2
NZS:3404 - 5.2.2.1
! /"#$ - #$ - #$2 ? #$ G s7r /"#$ ? @#$2 ! #0K@ Ley ! 1"$
for unsymmerical secton := weak axis bending exiss
Le ? Ley ! $0$)+ ritcal slenderness - minor y-axis %ax Le ? Ley ! $01K
---N
boom ange critcal
---N
Sec0on is co12act
Ls secton ! )01# Lsp ! Lsy ! @@ 31inor 6-a#is5
file:///conversion/tmp/scratch/362140164.xlsx
secton in y-axis mm)
NZS:3404 - 5.2.2.3 - 5.2.2.5
#
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!a# "CR
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Se!on moment apaity - major x-axis
%sx ! fyf G 'ex
NZS:3404 - e" 5.2.1
! "#$ G +,,",0# ? 1$$$$$$ %sx ! @",+0$+
k& m
T%sx ! @1"0)#
k& m
%Gx ! #$$
k& m
F= ! $0@"
--N
ok
Se!on moment apaity - minor y-axis
%sy ! fyf G 'ey
NZS:3404 - 5.1.2
! "#$ G )$@)#$,0#@ ? 1$$$$$$ %sy ! 1)$0#
k& m
T%sy ! 1@+,0,@
k& m
%Gy ! 1#$
k& m
F= ! $01@
--N
ok
Nominal member moment apaity o# se$ments - major x-axis only
P%bx ! 6m G 6s G %sx
Q!
%sx
NZS:3404 - e" 5.%.1.1&1'
6m ! 10@ 6s ! $0+ G /s7r / /%sx ? %oa2R@ J "2 - /%sx ? %oa22
NZS:3404 - e" 5.%.1.1&3'
%sx ! @",+0$#+ k& m NZS:3404 - (" 5.%.1.2 .e have an I secton wih une7ual ange /monosymmerc secton2 %oa ! s7r / /pi/2R@ G < G Iy ? HeR@22 G / s7r /G 92 J /pi/2R@ G < G Iw ? HeR@2 J /bxR@ G pi/2R@ G < G Iy ? ) ? HeR@2 2 J bx ? @ G s7r /pi/2R@ G < G Iy ? He R @2
Iy ! #0"
mm)
Iw ! df @ G b" G G 6 ? 1@
SS)* - 1++,
df ! disance beween ange cenroids 6 ! 1 ? /1 J /b ? bb2R" G / ? b22 ! 1 ? /1 J /)$$ ? )$12R" G /#$ ? #$22 ! $0# Iw ! /"#$ - #$ ? @ - #$ ? @2R@ G )$$R" G #$ G $0# ? 1@ ! 10@$$
mm+
< ! @$#$$$
m8a
! $$$$
m8a
9 ! /bb G bR" J b G R" J /d - - b2 G w2 ? " ! /)$1 G #$R" J )$$ G #$R" J /"#$ - #$ - #$2 G #$R"2 ? " ! )",K1+++0+,
mm)
He ! k G kr G kl G H
NZS:3404 - 5.%.3.1
! 101@ G 1 G 1 G +1+$ ! +KK0@
mm
Collowing propertes will be needed only if we have une7ual ange 4x ! $0 df G / /@ G Icy ? Iy2 - 12
NZS:3404 - 5.%.1.2.2
df ! "#$ - #$ ? @ - #$ ? @ ! "$$ Icy ! @++++++++0+,
mm mm)
4x ! $0 G "$$ G / /@ G @++++++++0+, ? #",K)@#$)01,2 - 12
file:///conversion/tmp/scratch/362140164.xlsx
+
! -@0$+
mm 9:; &A%<
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!a# "CR
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NZS:3404 - (" 5.%.1.2 =eference buckling momen %o ! s7r / pi/2R@ G < G Iy ? HeR@2 G / s7r / /G 92 J /pi/2R@ G < G Iw ? HeR@2 J /bxR@ G pi/2R@ G < G Iy ? ) ? HeR@2 2 2 J bx ? @ G s7r /pi/2R@ G < G Iy ? He R @2
! K#,K0,# k& m NZS:3404 - e" 5.%.1.1&3' 6s ! $0+ G / /s7r / /%sx ? %oa2R@ J "2 - /%sx ? %oa22 ! $0+ G / /s7r /@",+0$+ ? K#,K0,#2R@ J "2 - /@",+0$+? K#,K0,#2 2
! $0K 6m G 6s ! 10@ G $0K ! 10+"
--N
%bx ! 6m G 6s G %sx
Seg1ent is 78996 9atera9 restrained
Q!
%sx
! 10@ G $0K G @",+0$+ ! @",+0$+
k& m
T%bx ! @1"0)#
k& m
%Gx ! #$$
k& m
F= ! $0@"
--N
ok
Sear alla!ons &ns!/ened eb'
heck web sockiness
NZS:3404 - 5.11.2.1
dp ? w U @ ? /s7r /fc ? @#$22 @#$ ? #$ U @ ? /s7r /"#$ ? @#$22 # Q +K0"
--N
Web is stoc6
Bvu ! Bw Bw ! $0+ G fyw G Aw
NZS:3404 - 5.11.4.1
! $0+ G "#$ G /"#$ - #$ - #$2 G #$ ? 1$$$ ! @+@#
k&
Bb ! 6v G Bw
Q!
Bw
NZS:3404 - 5.11.5.1
6v ! /@ ? / /dp ? w2 G s7r /fyw ? @#$2 2 2R@ ! /@ ? / /"#$ - #$ - #$2 ? #$ G s7r /"#$ ? @#$ 2 2 2R@ ! 1K@011 Bb ! &?A
k&
TBvu ! $0K G @+@# ! @"+@0#
k&
BG ! $$
k&
F= ! $0")
--N
ok
Shear-bending ineracton %G ? T%sx ! $0@"
NZS:3404 - 5.12.2
Q
$0,# --N
Shear-bending ineracton need no o be considered
Bvm ! Bv G /@0@ - /10+%Gx ? T%sx22 ! @"+@0# G /@0@ - /10+ G #$$ ? $0K G @",+0$+2 2 ! @"+@0# BG ! $$
file:///conversion/tmp/scratch/362140164.xlsx
k& k&
,
F= ! $0")
file:///conversion/tmp/scratch/362140164.xlsx
--N
ok
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TEST RUN - VERIFY WIT !E!"ES
!a# "CR
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%&''
& A;IAL CA*ACITY - N,S'. C&< 3CO!*RESSION5 AN" C&= 3TENSION5 Tension member - assme end plate onne!on sed #or tension member n $
&ominal secton capaciy of ension member & ! min /Ag G fy* $0# G ke G An G fu2
NZS:3404 - .2.1
! min /#@##$ G "#$* $0# G 1 G #@##$ G )#$2 ? 1$$$ ! 1"K@0#
k&
T& ! $0K G 1"K@0# ! 1+##"0@#
k&
&G ! $
k&
no ension load
F= ! $
--N
ok
*ompression member - assme end plate onne!on sed no penetra!on n $
&ominal secton capaciy of compression member
NZS:3404 - e" %.2.1
&s ! kf G An G fyaverage
NZS:3404 - %.2.2
kf ! Ae ? Ag Ae ! Area of individual a plae elemens having eOectve widh be ! b G /Ley ? Le2 Q! b 3op ange Le ! )01) Ley ! 1) Ag op g ! @$$$$
for heavily welded seel secton ange mm@
Ae op g ! Ley ? Le G b G ! @$$$$
Q!
Ag op g
mm@
;oom ange Le ! )01# Ley ! 1) Ag bo g ! @$$#$
for heavily welded seel secton ange mm@
Ae bo g ! Ley ? Le G bb G b ! @$$#$
Q!
Ag bo g
mm@
.eb Le ! #0K@ Ley ! "# Ag web ! 1@#$$
for heavily welded seel secton ange mm@
Ae web ! Ley ? Le G /d--b2 G w ! 1@#$$
Q! Ag web
mm@
Ae oal ! @$$$$ J @$$#$ J 1@#$$ ! #@##$
mm@
kf ! #@##$ ? #@##$ ! 10$$$ &s ! 1 G #@##$ G /"#$ J "#$2 ? @ ? 1$$$ ! 1"K@0# T&s ! 1+##"0@#
k& k&
&G ! 1$$$$
file:///conversion/tmp/scratch/362140164.xlsx
K
F= ! $0+
file:///conversion/tmp/scratch/362140164.xlsx
--N
ok
1$
9:; &A%<
!
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TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
%&''
&ominal compression member capaciy %aMor x-axis He xx ! ke G H xx
NZS:3404 - %.3.2
! 1 G +1+$ ! +1+$
mm
Ln x ! /He xx ? rx2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /+1+$ ? 1"+012 G s7r /12 G s7r /"#$ ? @#$2 ! #"0#@ 6a ! @1$$ G /Ln x - 1"0#2 ? /Ln xR@ - 1#0" G Ln x J @$#$2 ! @1$$ G /#"0#@ - 1"0#2 ? /#"0#@R@ - 1#0" G #"0#@ J @$#$2 ! @$0#@ 6b ! $ Lx ! Ln x J 6a G 6b ! #"0#@ J @$0#@ G $ ! #"0#@ Vx ! max / $0$$"@+ G /Lx - 1"0#2 * $2 ! $01"$$$ Wx ! / / Lx ? K$2R@ J 1 J V 2 ? /@ G /Lx ? K$2R@2 ! / /#"0#@ ? K$2 R @ J 1 J $01"2 ? /@ G /#"0#@ ? K$2 R @2 ! @0$K$ 6c x ! Wx G / 1 - / s7r /1 - /K$ ? Wx ? Lx2R@ 2 2 ! @0$K G /1 - /s7r / 1 - /K$ ? @0$K ? #"0#@2R@ 2 2 ! $0)" %inor y-axis He yy ! ke G H yy
NZS:3404 - %.3.2
! 1 G +1+$ ! +1+$
mm
Ln y ! /He yy ? ry2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /+1+$ ? 1$1012 G s7r /12 G s7r /"#$ ? @#$2 ! ,@0$) 6a ! @1$$ G /Ln y - 1"0#2 ? /Ln yR@ - 1#0" G Ln y J @$#$2 ! @1$$ G /,@0$) - 1"0#2 ? /,@0$)R@ - 1#0" G ,@0$) J @$#$2 ! @$0$" 6b ! $ Ly ! Ln y J 6a G 6b ! ,@0$) J @$0$" G $ ! ,@0$) Vy ! max / $0$$"@+ G /Ly - 1"0#2 * $2 ! $01K1$$ Wy ! / / Ly ? K$2R@ J 1 J Vy 2 ? /@ G /Ly ? K$2R@2 ! / /,@0$) ? K$2 R @ J 1 J $01K12 ? /@ G /,@0$) ? K$2 R @2 ! 10)@K$ 6c y ! Wy G / 1 - / s7r /1 - /K$ ? Wy ? Ly2R@ 2 2
file:///conversion/tmp/scratch/362140164.xlsx
11
! 10)@K G /1 - /s7r / 1 - /K$ ? 10)@K ? ,@0$)2R@ 2 2 ! $0,"# 9:; &A%<
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TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
%&''
6c min ! min /6c x* 6c y2 ! $0,"# &c min ! 6c min G &s
NZS:3404 - %.3.3
! $0,"# G 1"K@0# ! 1"#10)K
k&
T&c ! 1@1++0+)
k&
&G ! 1$$$$
k&
F= ! $0@@
--N
ok
& CO!(INE" ACTIONS CA*ACITY 3N,S'.: C&>5 Si$ni6ant axial #ore e7
NZS:3404 - ,.1.4&a'
&G ! 1$$$$
k&
T&s ! 1+##"0@# &G ! $0+$
compression load
k& T&s
%Gy ! 1#$
--N
combined actons need o be checked
k& m minor y-axis bending exiss
T&cy ! 1@1++0+) &G ! $0@
NZS:3404 - ,.1.4&b'
k& m T&cy --N
combined actons need o be checked
8ased on l ,.1.4 e7 e need to e7 ombined a!ons9 ppliability o# alterna!e desi$n proisions
Is he member doubly symmericU
&
Is he secton compacU
D
Are he plae elemen slenderness for each plae no exceeding value from able 01U Balue Himi 3op g Le
!
)01)
Q
K
D
;o g Le
!
)01#
Q
K
D
.eb Le
!
)
Q
@
D
D
Is he member subMec o axial ensionU
&
is he form facor /kf2 uniyU
D
NZS:3404 - ,.1.5&a' NZS:3404 - ,.1.5&b'
D
NZS:3404 - ,.1.5&'
Foes he design compression force comply wih e7 010#U &G !
1$$$$
k&
T&s ! 1+##"0@#
k&
&G ? T&s U 10K - /d1 ? w G s7r /fyw ? @#$2 ? )#
D D
$0+ U 10K - /"$$ ? #$ G s7r / "#$ ? @#$2 ? )# $0+ Q
10,)
*e7 #ails alterna!e desi$n proision an;t be sed
file:///conversion/tmp/scratch/362140164.xlsx
1@
9:; &A%<
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TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
%&''
*ombined a!ons - se!on apaity
>niaxial x-axis bending %Gx ! #$$
k& m
NZS:3404 - ,.3.2.1
%rx ! %sx G /1 - &G ? T&s2 ! @",+0$+ G / 1 - 1$$$$ ? 1+##"0@#2 ! K)$0++
k& m
T%rx ! )+0#K
k& m
Alernatve design provision
can?t be 8sed
%rx ! 101 G %sx G /1 - &G ? T&s2 ! 11$K0K
NZS:3404 - ,.3.2.2
Q! %sx
k& m
T%rx ! KK0K
k& m
%rx used ! K)$0++
k& m
%Gx ! #$$
k& m
F= ! $0#K
--N
ok
>niaxial y-axis bending %Gy ! 1#$
k& m
NZS:3404 - ,.3.3.1
%ry ! %sy G /1 - &G ? T&s2 ! 1)$0# G / 1 - 1$$$$ ? 1+##"0@#2 ! ##,0+)
k& m
T%ry ! #$10
k& m
Alernatve design provision
can?t be 8sed
%ry ! 101K G %sy G /1 - &G ? T&s2R@ ! 1$+)0)
NZS:3404 - ,.3.3.2
Q! %sy
k& m
T%ry ! K#0$"
k& m
%ry aken ! ##,0+)
k& m
%Gy ! 1#$
k& m
F= ! $0"
--N
ok
;iaxial bending &G ? T&s J %Gx ? T%sx J %Gy ? T%sy Q!1
NZS:3404 - ,.3.4.1
1$$$$ ? 1+##"0@# J #$$ ? @",+0$+ J 1#$ ? 1)$0# Q! 1 ! $0K@1 F= ! $0K@1 Alernatve design provision
Q1 --N
ok
can?t be 8sed
/%Gx ? T%rx2RX J /%Gy ? T%ry2RX Q!1 X ! 10) J /&G ? T&s2 ! 10) J /1$$$$ ? 1+##"0@#2
NZS:3404 - ,.3.4.2
Q! @ Q! @
! @ /#$$ ? 11$K0K ? $0K2 R @ J /1#$ ? ##,0+)? $0K 2 R @ ! $0))
file:///conversion/tmp/scratch/362140164.xlsx
Q1
1"
F= !
file:///conversion/tmp/scratch/362140164.xlsx
--N
no alernatve design provision
1)
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TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
%&''
*ombined a!ons - member in-plane apaity
%aMor x-axis bending %ix ! %sx G /1 - &G ? T&c-x2* where
NZS:3404 - ,.4.2.2.1
T&c-x ! nominal member axial compression capaciy wih ke ! 1 Hex ! ke G H xx
NZS:3404 - %.3.2
! 1 G +1+$ ! +1+$
mm
Ln x ! /Hex ? rx2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /+1+$ ? 1"+012 G s7r /12 G s7r /"#$ ? @#$2 ! #"0#@ 6a ! @1$$ G /Ln x - 1"0#2 ? /Ln xR@ - 1#0" G Ln x J @$#$2 ! @1$$ G /#"0#@ - 1"0#2 ? /#"0#@R@ - 1#0" G #"0#@ J @$#$2 ! @$0#@ 6b ! $ Lx ! Ln x J 6a G 6b ! #"0#@ J @$0#@ G $ ! #"0#@ Vx ! max / $0$$"@+ G /Lx - 1"0#2 * $2 ! $01"$$$ Wx ! / / Lx ? K$2R@ J 1 J V 2 ? /@ G /Lx ? K$2R@2 ! / /#"0#@ ? K$2 R @ J 1 J $01"2 ? /@ G /#"0#@ ? K$2 R @2 ! @0$K$ 6c x ! Wx G / 1 - / s7r /1 - /K$ ? Wx ? Lx2R@ 2 2 ! @0$K G /1 - /s7r / 1 - /K$ ? @0$K ? #"0#@2R@ 2 2 ! $0)" &c-x ! $0)" G 1"K@0# ! 1##$)0
k&
T&c-x ! 1"K#)0"K
k&
%ix ! @",+0$+ G /1 - 1$$$$ ? 1"K#)0"K2 ! +,"0"" Alernatve design provision
k& m can?t be 8sed
NZS:3404 - ,.4.2.2.2
%ix ! %sx G / /1 - / / /1 J 4m2 ? @2R"2 G /1 - &G ? T&cx2 J 101 G / / /1 J 4m2 ? @2R"2 G s7r /1 - &G ? T&cx2 2 Q!%rx ! @",+0$+ G / /1 - / / /1 J $2 ? @2R"2 G /1 - 1$$$$ ? 1"K#)0"K2 J 101 G / / /1 J $2 ? @2R"2 G s7r /1 - 1$$$$ ? 1"K#)0"K2 2 Q! %rx ! ,,#0,"
k& m
%ix aken ! +,"0""
k& m
T%ix ! +$+
k& m
%Gx ! #$$
k& m
F= ! $0"
--N
file:///conversion/tmp/scratch/362140164.xlsx
ok
1#
9:; &A%<
!
3&
?@?@$1,
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8 SECTION FAILS
TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
%&''
*ombined a!ons - member in-plane apaity
%aMor y-axis bending %iy ! %sy G /1 - &G ? T&c-y2* where
NZS:3404 - ,.4.2.2.1
T&c-y ! nominal member axial compression capaciy wih ke ! 1 Hey ! ke G H yy
NZS:3404 - %.3.2
! 1 G +1+$ ! +1+$
mm
Ln y ! /Hey ? ry2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /+1+$ ? 1$1012 G s7r /12 G s7r /"#$ ? @#$2 ! ,@0$) 6a ! @1$$ G /Ln y - 1"0#2 ? /Ln yR@ - 1#0" G Ln y J @$#$2 ! @1$$ G /,@0$) - 1"0#2 ? /,@0$)R@ - 1#0" G ,@0$) J @$#$2 ! @$0$" 6b ! $ Ly ! Ln y J 6a G 6b ! ,@0$) J @$0$" G $ ! ,@0$) Vy ! max / $0$$"@+ G /Ly - 1"0#2 * $2 ! $01K1$$ Wy ! / / Ly ? K$2R@ J 1 J V 2 ? /@ G /Ly ? K$2R@2 ! / /,@0$) ? K$2 R @ J 1 J $01K12 ? /@ G /,@0$) ? K$2 R @2 ! 10)@K$ 6c y ! Wy G / 1 - / s7r /1 - /K$ ? Wy ? Ly2R@ 2 2 ! 10)@K G /1 - /s7r / 1 - /K$ ? 10)@K ? ,@0$)2R@ 2 2 ! $0,"# &c-y ! $0,"# G 1"K@0# ! 1"#10)K
k&
T&c-y ! 1@1++0+)
k&
%iy ! 1)$0# G /1 - 1$$$$ ? 1@1++0+)2 ! @#$0) Alernatve design provision
k& m can?t be 8sed
NZS:3404 - ,.4.2.2.2
%iy ! %sy G / /1 - / / /1 J 4m2 ? @2R"2 G /1 - &G ? T&cy2 J 101 G / / /1 J 4m2 ? @2R"2 G s7r /1 - &G ? T&cy2 2 Q!%ry ! 1)$0# G / /1 - / / /1 J $2 ? @2R"2 G /1 - 1$$$$ ? 1@1++0+)2 J 101 G / / /1 J $2 ? @2R"2 G s7r /1 - 1$$$$ ? 1@1++0+)2 2 Q! %ry ! "$,01+
k& m
%iy aken ! @#$0)
k& m
T%iy ! @@#0,+
k& m
%Gy ! 1#$
k& m
F= ! $0++
--N
file:///conversion/tmp/scratch/362140164.xlsx
ok
1+
9:; &A%<
!
3&
?@?@$1,
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8 SECTION FAILS
TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
%&''
*ombined a!ons - member ot-o#-plane apaity
heck of ou-of-plane member capaciy needs o be done only when member is no fully laerally resrained0 6m G 6s ! 10+"
--N
Segmen is fully laeral resrained
--N
&o need o check ou-of-plane member capaciy
Cor compression member( %ox ! %bx G /1 - &G ? T&c-y2
NZS:3404 - ,.4.4.1.1
! @",+0$+ G /1 - 1$$$$ ? 1@1++0+)2 ! )@"01"
k& m
Alernatve design provision
can?t be 8sed
NZS:3404 - ,.4.4.1.2
%ox ! 6bc G %bxo G s7r / /1 - &G ? T&cy2 G /1 - &G ? T&oY2 2 6bc ! 1 ? / / /1 - 4m2 ? @2 J/ /1 J 4m2 ? @2R"2 G /$0) - $0@" G &G ? T&cy2 ! 1 ? / / /1 - $2 ? @2 J/ /1 J $2 ? @2R"2 G /$0) - $0@" G 1$$$$ ? 1@1++0+)2 ! 10K %bxo ! 6m G 6s G %sx
--N 6m is aken as uniy
! 1 G $0K G @",+0$+ ! @1"0)#
k& m
&oY ! / G 9 J /pi/2R@ G < G Iw ? HYR@2 2 ? / /Ix J Iy2 ? A2 ! $$$$ 9 ! )",K1+++0+, Iw ! 10@
%pa mm) mm+
Ixx ! K,)#,1)+0+), mm) Iyy ! #",K)@#$)01,
mm)
HY ! +1+$ mm &oY ! /$$$$ G )",K1+++0+, J /pi/2R@ G @$#$$$ G 1@$$$$$$$$$$$$ ? ",K)#+$$2 2 ? / /K,)#,1)+0+)+++, J #",K)@#$)01,2 ? #@##$2 ? 1$$$ ! 1)"K)0"" k& T&oY ! 1@K##"0#
k&
%ox ! 10K G @1"0)# G s7r/ /1 - 1$$$$ ? 1@1++0+)2 G /1 - 1$$$$ ? 1@K##"0#2 2 Q! %rx ! K)$0++
k& m
%ox aken !
k& m
%Gx !
k&m
F= !
--N
Cully laerally resrained - no need o check his
;iaxial bending for compression member
NZS:3404 - ,.4.5.1
/%Gx ? T%cx2R10) J /%Gy ? T%iy2R10) Q!1 %Gx ! #$$
k& m
%cx ! +,"0""
k& m
%Gy ! 1#$
k& m
%iy ! @#$0)
k& m
/#$$ ? $0K ? +,"0""2R10) J /1#$ ? $0K ? @#$0)2R10) Q!1 F= ! 10""
file:///conversion/tmp/scratch/362140164.xlsx
--N
no ok
1,
9:; &A%<
!
3&
?@?@$1,
S>;9<3
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B<=ICD .I3E %<%F
;D
!
.8 SECTION FAILS
TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
%&''
Cor ension member( %ox ! %bx G /1 - &G ? T&2 Q! %rx
NZS:3404 - ,.4.4.2
! @",+0$+ G /1 - 1$$$$ ? $0K ? 1"K@0#2 Q! %rx ! K)$0++
k& m
T%ox !
k& m
%Gx !
k& m
F= !
--N
no ension load
;iaxial bending for ension member
NZS:3404 - ,.4.4.2
/%Gx ? T%x2R10) J /%Gy ? T%ry2R10) Q!1 %Gx !
k& m
%x !
k& m
%Gy !
k& m
%ry !
k& m
/ ? $0K ? 2R10) J / ? $0K ? 2R10) Q!1 F= !
file:///conversion/tmp/scratch/362140164.xlsx
--N
no ension load
1
9:; &A%<
!
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?@?@$1,
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.8
TEST RUN - VERIFY WIT !E!"ES %& LOA"S AN" !E!(ER CON"ITION 1#$ &G ! k&
"$$
%Gx ! %Gy !
$$
BG !
!a# "CR
$
.&@
H xx
!
"$$$
mm
fyf
!
"#$
m8a
k& m
H yy
!
"$$$
mm
fyw
!
"#$
m8a
k& m
H
!
"$$
mm
fu
!
)#$
m8a
<
!
k&
@$#$$$ m8a
ompressed ange %Gm !
k& m
k
!
101@
%G@ !
k& m
kl
!
1
%G" !
k& m
kr
!
1
%G) ! 6m !
k& m
ke 6m
!
1
10$$
!
!
;:33:%
4m-x
!
$
4m-y
!
$
Ghis will overwrie he value on he le
)& SECTION *RO*ERTIES
d !
#$$
mm
A
!
1$+$
mm@
cx
!
$
mm
b !
@,#
mm
x
!
1",0#
mm
cy
!
-+"01
mm
bb !
1"$
mm
y
!
"1"01 mm
Iw
! )0##
!
1+
mm
Ixx
!
"0K+
Sx
!
101
b !
1@
mm
Iyy
!
"0$$
Sy
!
"0+#
w !
1$
mm
9
!
+0$
'x
!
10@+
rx
!
1K@0)
'y
!
@01
ry
!
#@0K,
3ype !
.;
'& (EN"IN+ AN" SEAR CA*ACITY - N,S'. C&/ Major x-axis slenderness parameter
3op Clange slenderness parameer Ls Le ! b ? G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /@,# - 1$2 ? @ ? 1+ G s7r /"#$ ? @#$2 ! K0 Ley ! 1)
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $0, ;oom Clange slenderness parameer Ls Le ! bb ? b G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /1"$ - 1$2 ? @ ? 1@ G s7r /"#$ ? @#$2 ! #0K@ Ley ! 1)
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $0)@" .eb slenderness parameer Ls Le ! dw ? w G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /#$$ - 1+ - 1@2 ? 1$ G s7r /"#$ ? @#$2 ! ##0# Ley ! 1"$
file:///conversion/tmp/scratch/362140164.xlsx
for unsymmerical secton := weak axis bending exiss
1K
Le ? Ley ! $0)" 9:; &A%<
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3&
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B<=ICD .I3E %<%F
;D
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.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
ritcal slenderness - maMor x-axis %ax Le ? Ley ! $0,
---N
op ange critcal
---N
Sec0on is non-co12act
Ls secton ! K0 Lsp ! Lsy ! 1) 31a4or #-a#is5
secton in x-axis mm)
NZS:3404 - 5.2.2.3 - 5.2.2.5
Le ! b ? G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
'ex ! 10+))
3op Clange slenderness parameer Ls ! /@,# - 1$2 ? @ ? 1+ G s7r /"#$ ? @#$2 ! K0 Ley ! @@
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $0))# ;oom Clange slenderness parameer Ls Le ! bb ? b G s7r /fy ? @#$2
NZS:3404 - 5.2.2.1
! /1"$ - 1$2 ? @ ? 1@ G s7r /"#$ ? @#$2 ! #0K@ Ley ! @@
for heavily welded seel secton ange
NZS:3404 - Table 5.2
Le ? Ley ! $0@+K .eb slenderness parameer Ls Le ! dw ? w G s7r /fyw ? @#$2
NZS:3404 - 5.2.2.1
! /#$$ - 1+ - 1@2 ? 1$ G s7r /"#$ ? @#$2 ! ##0# Ley ! 1"$
for unsymmerical secton := weak axis bending exiss
Le ? Ley ! $0)" ritcal slenderness - minor y-axis %ax Le ? Ley ! $0))#
---N
op ange critcal
---N
Sec0on is non-co12act
Ls secton ! K0 Lsp ! Lsy ! @@ 31inor 6-a#is5
file:///conversion/tmp/scratch/362140164.xlsx
secton in y-axis mm)
NZS:3404 - 5.2.2.3 - 5.2.2.5
@$
9:; &A%<
!
3&
S>;9<3
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;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
Se!on moment apaity - major x-axis
%sx ! fyf G 'ex
NZS:3404 - e" 5.2.1
! "#$ G 1+)"#),0$@ ? 1$$$$$$ %sx ! #,#0@)
k& m
T%sx ! #1,0,@
k& m
%Gx ! "$$
k& m
F= ! $0#
--N
ok
Se!on moment apaity - minor y-axis
%sy ! fyf G 'ey
NZS:3404 - 5.1.2
! "#$ G "1@+0#" ? 1$$$$$$ %sy ! 1$K0#1 T%sy ! K0#+
k& m k& m
%Gy ! $
k& m
F= ! $
--N
ok
Nominal member moment apaity o# se$ments - major x-axis only
P%bx ! 6m G 6s G %sx
Q!
%sx
NZS:3404 - e" 5.%.1.1&1'
6m ! 1 6s ! $0+ G /s7r / /%sx ? %oa2R@ J "2 - /%sx ? %oa22
NZS:3404 - e" 5.%.1.1&3'
%sx ! #,#0@))) k& m NZS:3404 - (" 5.%.1.2 .e have an I secton wih une7ual ange /monosymmerc secton2 %oa ! s7r / /pi/2R@ G < G Iy ? HeR@22 G / s7r /G 92 J /pi/2R@ G < G Iw ? HeR@2 J /bxR@ G pi/2R@ G < G Iy ? ) ? HeR@2 2 J bx ? @ G s7r /pi/2R@ G < G Iy ? He R @2
Iy ! "0$$
mm)
Iw ! df @ G b" G G 6 ? 1@
SS)* - 1++,
df ! disance beween ange cenroids 6 ! 1 ? /1 J /b ? bb2R" G / ? b22 ! 1 ? /1 J /@,# ? 1"$2R" G /1+ ? 1@22 ! $0$, Iw ! /#$$ - 1+ ? @ - 1@ ? @2R@ G @,#R" G 1+ G $0$, ? 1@ ! )0##
mm+
< ! @$#$$$
m8a
! $$$$
m8a
9 ! /bb G bR" J b G R" J /d - - b2 G w2 ? " ! /1"$ G 1@R" J @,# G 1+R" J /#$$ - 1+ - 1@2 G 1$R"2 ? " ! +$,+$
mm)
He ! k G kr G kl G H
NZS:3404 - 5.%.3.1
! 101@ G 1 G 1 G "$$ ! ""+
mm
Collowing propertes will be needed only if we have une7ual ange 4x ! $0 df G / /@ G Icy ? Iy2 - 12
NZS:3404 - 5.%.1.2.2
df ! #$$ - 1+ ? @ - 1@ ? @ ! )+
mm
Icy ! @1K,$$$
mm)
4x ! $0 G )+ G / /@ G @1K,$$$ ? @KK+##$$2 - 12
file:///conversion/tmp/scratch/362140164.xlsx
@1
! -""10,K
mm 9:; &A%<
!
3&
S>;9<3
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B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
NZS:3404 - (" 5.%.1.2 =eference buckling momen %o ! s7r / pi/2R@ G < G Iy ? HeR@2 G / s7r / /G 92 J /pi/2R@ G < G Iw ? HeR@2 J /bxR@ G pi/2R@ G < G Iy ? ) ? HeR@2 2 2 J bx ? @ G s7r /pi/2R@ G < G Iy ? He R @2
! @@1##0#) k& m NZS:3404 - e" 5.%.1.1&3' 6s ! $0+ G / /s7r / /%sx ? %oa2R@ J "2 - /%sx ? %oa22 ! $0+ G / /s7r /#,#0@) ? @@1##0#)2R@ J "2 - /#,#0@)? @@1##0#)2 2
! 10$@ 6m G 6s ! 1 G 10$@ ! 10$@
--N
%bx ! 6m G 6s G %sx
Seg1ent is 78996 9atera9 restrained
Q!
%sx
! 1 G 10$@ G #,#0@) ! #,#0@)
k& m
T%bx ! #1,0,@
k& m
%Gx ! "$$
k& m
F= ! $0#
--N
ok
Sear alla!ons &ns!/ened eb'
heck web sockiness
NZS:3404 - 5.11.2.1
dp ? w U @ ? /s7r /fc ? @#$22 ),@ ? 1$ U @ ? /s7r /"#$ ? @#$22 ),0@ Q +K0"
--N
Web is stoc6
Bvu ! Bw Bw ! $0+ G fyw G Aw
NZS:3404 - 5.11.4.1
! $0+ G "#$ G /#$$ - 1+ - 1@2 G 1$ ? 1$$$ ! KK10@
k&
Bb ! 6v G Bw
Q!
Bw
NZS:3404 - 5.11.5.1
6v ! /@ ? / /dp ? w2 G s7r /fyw ? @#$2 2 2R@ ! /@ ? / /#$$ - 1+ - 1@2 ? 1$ G s7r /"#$ ? @#$ 2 2 2R@ ! @01+ Bb ! &?A
k&
TBvu ! $0K G KK10@ ! K@0$
k&
BG ! $$
k&
F= ! $0K$
--N
ok
Shear-bending ineracton %G ? T%sx ! $0#
NZS:3404 - 5.12.2
Q
$0,# --N
Shear-bending ineracton need no o be considered
Bvm ! Bv G /@0@ - /10+%Gx ? T%sx22 ! K@0$ G /@0@ - /10+ G "$$ ? $0K G #,#0@)2 2 ! K@0$ BG ! $$
file:///conversion/tmp/scratch/362140164.xlsx
k& k&
@@
F= ! $0K
file:///conversion/tmp/scratch/362140164.xlsx
--N
ok
@"
9:; &A%<
!
3&
S>;9<3
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B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
& A;IAL CA*ACITY - N,S'. C&< 3CO!*RESSION5 AN" C&= 3TENSION5 Tension member - assme end plate onne!on sed #or tension member n $
&ominal secton capaciy of ension member & ! min /Ag G fy* $0# G ke G An G fu2
NZS:3404 - .2.1
! min /1$+$ G "#$* $0# G 1 G 1$+$ G )#$2 ? 1$$$ ! ","
k&
T& ! $0K G "," ! ""+)0@
k&
&G ! $
k&
no ension load
F= ! $
--N
ok
*ompression member - assme end plate onne!on sed no penetra!on n $
&ominal secton capaciy of compression member
NZS:3404 - e" %.2.1
&s ! kf G An G fyaverage
NZS:3404 - %.2.2
kf ! Ae ? Ag Ae ! Area of individual a plae elemens having eOectve widh be ! b G /Ley ? Le2 Q! b 3op ange Le ! K0 Ley ! 1) Ag op g ! ))$$
for heavily welded seel secton ange mm@
Ae op g ! Ley ? Le G b G ! ))$$
Q!
Ag op g
mm@
;oom ange Le ! #0K@ Ley ! 1) Ag bo g ! 1#+$
for heavily welded seel secton ange mm@
Ae bo g ! Ley ? Le G bb G b ! 1#+$
Q!
Ag bo g
mm@
.eb Le ! ##0# Ley ! "# Ag web ! ),@$
for heavily welded seel secton ange mm@
Ae web ! Ley ? Le G /d--b2 G w ! @K#,0K@
Q! Ag web
mm@
Ae oal ! ))$$ J 1#+$ J @K#,0K@ ! K1,0K@
mm@
kf ! K1,0K@ ? 1$+$ ! $0"# &s ! $0"# G 1$+$ G /"#$ J "#$2 ? @ ? 1$$$ ! "1@10@"
k&
T&s ! @$K011
k&
&G ! 1#$
file:///conversion/tmp/scratch/362140164.xlsx
@)
F= ! $0$#
file:///conversion/tmp/scratch/362140164.xlsx
--N
ok
@#
9:; &A%<
!
3&
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
&ominal compression member capaciy %aMor x-axis He xx ! ke G H xx
NZS:3404 - %.3.2
! 1 G "$$$ ! "$$$
mm
Ln x ! /He xx ? rx2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /"$$$ ? 1K@0)2 G s7r /$0"#2 G s7r /"#$ ? @#$2 ! 1+0# 6a ! @1$$ G /Ln x - 1"0#2 ? /Ln xR@ - 1#0" G Ln x J @$#$2 ! @1$$ G /1+0# - 1"0#2 ? /1+0#R@ - 1#0" G 1+0# J @$#$2 ! "0"K 6b ! $0# Lx ! Ln x J 6a G 6b ! 1+0# J "0"K G $0# ! 10## Vx ! max / $0$$"@+ G /Lx - 1"0#2 * $2 ! $0$1+$$ Wx ! / / Lx ? K$2R@ J 1 J V 2 ? /@ G /Lx ? K$2R@2 ! / /10## ? K$2 R @ J 1 J $0$1+2 ? /@ G /10## ? K$2 R @2 ! 1@0)#$ 6c x ! Wx G / 1 - / s7r /1 - /K$ ? Wx ? Lx2R@ 2 2 ! 1@0)# G /1 - /s7r / 1 - /K$ ? 1@0)# ? 10##2R@ 2 2 ! $0K) %inor y-axis He yy ! ke G H yy
NZS:3404 - %.3.2
! 1 G "$$$ ! "$$$
mm
Ln y ! /He yy ? ry2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /"$$$ ? #@0K,2 G s7r /$0"#2 G s7r /"#$ ? @#$2 ! +10@" 6a ! @1$$ G /Ln y - 1"0#2 ? /Ln yR@ - 1#0" G Ln y J @$#$2 ! @1$$ G /+10@" - 1"0#2 ? /+10@"R@ - 1#0" G +10@" J @$#$2 ! @$0+1 6b ! $0# Ly ! Ln y J 6a G 6b ! +10@" J @$0+1 G $0# ! ,10#) Vy ! max / $0$$"@+ G /Ly - 1"0#2 * $2 ! $01K$$ Wy ! / / Ly ? K$2R@ J 1 J Vy 2 ? /@ G /Ly ? K$2R@2 ! / /,10#) ? K$2 R @ J 1 J $01K2 ? /@ G /,10#) ? K$2 R @2 ! 10))1$ 6c y ! Wy G / 1 - / s7r /1 - /K$ ? Wy ? Ly2R@ 2 2
file:///conversion/tmp/scratch/362140164.xlsx
@+
! 10))1 G /1 - /s7r / 1 - /K$ ? 10))1 ? ,10#)2R@ 2 2 ! $0," 9:; &A%<
!
3&
?@?@$1,
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
!a# "CR
$
.&@
6c min ! min /6c x* 6c y2 ! $0," &c min ! 6c min G &s
NZS:3404 - %.3.3
! $0," G "1@10@" ! @"$"0),
k&
T&c ! @$,"01@
k&
&G ! 1#$
k&
F= ! $0$,@
--N
ok
& CO!(INE" ACTIONS CA*ACITY 3N,S'.: C&>5 Si$ni6ant axial #ore e7
NZS:3404 - ,.1.4&a'
&G ! 1#$
k&
T&s ! @$K011 &G ! $0$#
compression load
k& T&s
%Gy ! $
--N
combined actons need o be checked
k& m no minor y-axis bending
T&cy ! @$,"01@ &G ! $0$,
NZS:3404 - ,.1.4&b'
k& m T&cy --N
combined actons need o be checked
8ased on l ,.1.4 e7 e need to e7 ombined a!ons9 ppliability o# alterna!e desi$n proisions
Is he member doubly symmericU
&
Is he secton compacU
&
Are he plae elemen slenderness for each plae no exceeding value from able 01U Balue Himi 3op g Le
!
K0
N
K
&
;o g Le
!
#0K@
Q
K
D
.eb Le
!
)
Q
@
D
&
Is he member subMec o axial ensionU
&
is he form facor /kf2 uniyU
&
NZS:3404 - ,.1.5&a' NZS:3404 - ,.1.5&b'
&
NZS:3404 - ,.1.5&'
Foes he design compression force comply wih e7 010#U &G !
1#$
k&
T&s !
@$K011
k&
&G ? T&s U 10K - /d1 ? w G s7r /fyw ? @#$2 ? )#
D D
$0$# U 10K - /)+ ? 1$ G s7r / "#$ ? @#$2 ? )# $0$# Q
$0+@
*e7 #ails alterna!e desi$n proision an;t be sed
file:///conversion/tmp/scratch/362140164.xlsx
@,
9:; &A%<
!
3&
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
*ombined a!ons - se!on apaity
>niaxial x-axis bending %Gx ! "$$
k& m
NZS:3404 - ,.3.2.1
%rx ! %sx G /1 - &G ? T&s2 ! #,#0@) G / 1 - 1#$ ? @$K0112 ! #))0#@
k& m
T%rx ! )K$0$,
k& m
Alernatve design provision
can?t be 8sed
%rx ! 101 G %sx G /1 - &G ? T&s2 ! #,#0@)
k& m
T%rx ! #1,0,@
k& m
%rx used ! #))0#@
k& m
%Gx ! "$$
k& m
F= ! $0+1
--N
NZS:3404 - ,.3.2.2
Q! %sx
ok
>niaxial y-axis bending %Gy ! $
k& m
NZS:3404 - ,.3.3.1
%ry ! %sy G /1 - &G ? T&s2 ! 1$K0#1 G / 1 - 1#$ ? @$K0112 ! 1$"0++ T%ry ! K"0@K Alernatve design provision
k& m k& m can?t be 8sed
%ry ! 101K G %sy G /1 - &G ? T&s2R@ ! 1$K0#1 T%ry ! K0#+
NZS:3404 - ,.3.3.2
Q! %sy
k& m k& m
%ry aken ! 1$"0++
k& m
%Gy ! $
k& m
F= ! $
--N
ok
;iaxial bending &G ? T&s J %Gx ? T%sx J %Gy ? T%sy Q!1
NZS:3404 - ,.3.4.1
1#$ ? @$K011 J "$$ ? #,#0@) J ? 1$K0#1 Q! 1 ! $0#,# F= ! Alernatve design provision
Q1 --N
no minor y-axis bending
can?t be 8sed
/%Gx ? T%rx2RX J /%Gy ? T%ry2RX Q!1 X ! 10) J /&G ? T&s2 ! 10) J /1#$ ? @$K0112
NZS:3404 - ,.3.4.2
Q! @ Q! @
! 10)# /"$$ ? #,#0@) ? $0K2 R 10)# J / ? 1$"0++? $0K 2 R 10)# ! $0)K
file:///conversion/tmp/scratch/362140164.xlsx
Q1
@
F= !
file:///conversion/tmp/scratch/362140164.xlsx
--N
no minor y-axis bending
@K
9:; &A%<
!
3&
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
*ombined a!ons - member in-plane apaity
%aMor x-axis bending %ix ! %sx G /1 - &G ? T&c-x2* where
NZS:3404 - ,.4.2.2.1
T&c-x ! nominal member axial compression capaciy wih ke ! 1 Hex ! ke G H xx
NZS:3404 - %.3.2
! 1 G "$$$ ! "$$$
mm
Ln x ! /Hex ? rx2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /"$$$ ? 1K@0)2 G s7r /$0"#2 G s7r /"#$ ? @#$2 ! 1+0# 6a ! @1$$ G /Ln x - 1"0#2 ? /Ln xR@ - 1#0" G Ln x J @$#$2 ! @1$$ G /1+0# - 1"0#2 ? /1+0#R@ - 1#0" G 1+0# J @$#$2 ! "0"K 6b ! $0# Lx ! Ln x J 6a G 6b ! 1+0# J "0"K G $0# ! 10## Vx ! max / $0$$"@+ G /Lx - 1"0#2 * $2 ! $0$1+$$ Wx ! / / Lx ? K$2R@ J 1 J V 2 ? /@ G /Lx ? K$2R@2 ! / /10## ? K$2 R @ J 1 J $0$1+2 ? /@ G /10## ? K$2 R @2 ! 1@0)#$ 6c x ! Wx G / 1 - / s7r /1 - /K$ ? Wx ? Lx2R@ 2 2 ! 1@0)# G /1 - /s7r / 1 - /K$ ? 1@0)# ? 10##2R@ 2 2 ! $0K) &c-x ! $0K) G "1@10@" ! "$,10@K
k&
T&c-x ! @,+)01+
k&
%ix ! #,#0@) G /1 - 1#$ ? @,+)01+2 ! #))0$@ Alernatve design provision
k& m can?t be 8sed
NZS:3404 - ,.4.2.2.2
%ix ! %sx G / /1 - / / /1 J 4m2 ? @2R"2 G /1 - &G ? T&cx2 J 101 G / / /1 J 4m2 ? @2R"2 G s7r /1 - &G ? T&cx2 2 Q!%rx ! #,#0@) G / /1 - / / /1 J $2 ? @2R"2 G /1 - 1#$ ? @,+)01+2 J 101 G / / /1 J $2 ? @2R"2 G s7r /1 - 1#$ ? @,+)01+2 2 Q! %rx ! #))0#@
k& m
%ix aken ! #))0$@
k& m
T%ix ! )K0+@
k& m
%Gx ! "$$
k& m
F= ! $0+1
--N
file:///conversion/tmp/scratch/362140164.xlsx
ok
"$
9:; &A%<
!
3&
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
*ombined a!ons - member in-plane apaity
%aMor y-axis bending %iy ! %sy G /1 - &G ? T&c-y2* where
NZS:3404 - ,.4.2.2.1
T&c-y ! nominal member axial compression capaciy wih ke ! 1 Hey ! ke G H yy
NZS:3404 - %.3.2
! 1 G "$$$ ! "$$$
mm
Ln y ! /Hey ? ry2 G s7r /kf2 G s7r /fy ? @#$2
NZS:3404 - %.3.3
! /"$$$ ? #@0K,2 G s7r /$0"#2 G s7r /"#$ ? @#$2 ! +10@" 6a ! @1$$ G /Ln y - 1"0#2 ? /Ln yR@ - 1#0" G Ln y J @$#$2 ! @1$$ G /+10@" - 1"0#2 ? /+10@"R@ - 1#0" G +10@" J @$#$2 ! @$0+1 6b ! $0# Ly ! Ln y J 6a G 6b ! +10@" J @$0+1 G $0# ! ,10#) Vy ! max / $0$$"@+ G /Ly - 1"0#2 * $2 ! $01K$$ Wy ! / / Ly ? K$2R@ J 1 J V 2 ? /@ G /Ly ? K$2R@2 ! / /,10#) ? K$2 R @ J 1 J $01K2 ? /@ G /,10#) ? K$2 R @2 ! 10))1$ 6c y ! Wy G / 1 - / s7r /1 - /K$ ? Wy ? Ly2R@ 2 2 ! 10))1 G /1 - /s7r / 1 - /K$ ? 10))1 ? ,10#)2R@ 2 2 ! $0," &c-y ! $0," G "1@10@" ! @"$"0),
k&
T&c-y ! @$,"01@
k&
%iy ! 1$K0#1 G /1 - 1#$ ? @$,"01@2 ! 1$10#K Alernatve design provision
k& m can?t be 8sed
NZS:3404 - ,.4.2.2.2
%iy ! %sy G / /1 - / / /1 J 4m2 ? @2R"2 G /1 - &G ? T&cy2 J 101 G / / /1 J 4m2 ? @2R"2 G s7r /1 - &G ? T&cy2 2 Q!%ry ! 1$K0#1 G / /1 - / / /1 J $2 ? @2R"2 G /1 - 1#$ ? @$,"01@2 J 101 G / / /1 J $2 ? @2R"2 G s7r /1 - 1#$ ? @$,"01@2 2 Q! %ry ! 1$"0++
k& m
%iy aken ! 1$10#K
k& m
T%iy ! K10)"
k& m
%Gy ! $
k& m
F= ! $
--N
file:///conversion/tmp/scratch/362140164.xlsx
ok
"1
9:; &A%<
!
3&
S>;9<3
!
B<=ICD .I3E %<%F
;D
!
.8
TEST RUN - VERIFY WIT !E!"ES
?@?@$1,
!a# "CR
$
.&@
*ombined a!ons - member ot-o#-plane apaity
heck of ou-of-plane member capaciy needs o be done only when member is no fully laerally resrained0 6m G 6s ! 10$@
--N
Segmen is fully laeral resrained
--N
&o need o check ou-of-plane member capaciy
Cor compression member( %ox ! %bx G /1 - &G ? T&c-y2
NZS:3404 - ,.4.4.1.1
! #,#0@) G /1 - 1#$ ? @$,"01@2 ! #""0+@
k& m
Alernatve design provision
can?t be 8sed
NZS:3404 - ,.4.4.1.2
%ox ! 6bc G %bxo G s7r / /1 - &G ? T&cy2 G /1 - &G ? T&oY2 2 6bc ! 1 ? / / /1 - 4m2 ? @2 J/ /1 J 4m2 ? @2R"2 G /$0) - $0@" G &G ? T&cy2 ! 1 ? / / /1 - $2 ? @2 J/ /1 J $2 ? @2R"2 G /$0) - $0@" G 1#$ ? @$,"01@2 ! 10@# %bxo ! 6m G 6s G %sx
--N 6m is aken as uniy
! 1 G 10$@ G #,#0@) ! #+0,)
k& m
&oY ! / G 9 J /pi/2R@ G < G Iw ? HYR@2 2 ? / /Ix J Iy2 ? A2 ! $$$$ 9 ! +$,+$
%pa mm)
Iw ! )#)++@,,#$$ mm+ Ixx ! "K#+K1)+K0@"@ mm) Iyy ! @KK+##$$
mm)
HY ! "$$ mm &oY ! /$$$$ G +$,+$ J /pi/2R@ G @$#$$$ G )#)++@,,#$$ ? K$$$$2 2 ? / /"K#+K1)+K0@"@ J @KK+##$$2 ? 1$+$2 ? 1$$$ ! @#K@$0+#
k&
T&oY ! @"""0#K
k&
%ox ! 10@# G #+0,) G s7r/ /1 - 1#$ ? @$,"01@2 G /1 - 1#$ ? @"""0#K2 2 Q! %rx ! #))0#@
k& m
%ox aken !
k& m
%Gx !
k&m
F= !
--N
Cully laerally resrained - no need o check his
;iaxial bending for compression member
NZS:3404 - ,.4.5.1
/%Gx ? T%cx2R10) J /%Gy ? T%iy2R10) Q!1 %Gx ! "$$
k& m
%cx ! #))0$@
k& m
%Gy ! $
k& m
%iy ! 1$10#K
k& m
/"$$ ? $0K ? #))0$@2R10) J /$ ? $0K ? 1$10#K2R10) Q!1 F= !
file:///conversion/tmp/scratch/362140164.xlsx
--N
&o biaxial acton
"@