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    ! "#$% ' ( ) *+, - . / ( 0 , 1 2. - 2" 2 3 #. , +24 526 0 ( . 5- 2. $#$% / , . +7 , +. 24 / , 26#4#, 8

    9 ( $ : #- ) #2$

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    Annual Stability Conference11 Sessions35+ Papers

    Rm. Texas 3-4

    Stability Fun!

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    ;

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    /,.+7,+.- (0 /,--4 '(+."-"G2,-.#24

    *.("K 7($"

    ' ( )

    * . - " " # ( $

    I-$"#($

    L/>59M>

    N42,-O#.H-."

    '()6#$-H! # $ /8",-)"

    '($$-7,#($"! K %

    '()*("#,-'($$-7,#($"

    $

    P$,.(H+7,#($

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    /,.+7,+.- (0 /,--4 '(+."-"

    Q=2, H(-",=- 7(+."- -)*=2"#R-S

    T-=2

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    /,.+7,+.- (0 /,--4 '(+."-"

    Q=( 2.-8(+. ",+H-$,"S

    /,.+7,+.24U$%#$--.#$%

    '($",.+7,#($G2$2%-)-$,

    L.7=#,-7,+.-

    L.7=#,-7,+.24U$%#$--.#$%

    !$H-.%.2H+2,- O.2H+2,- /,+H-$,

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    /,.+7,+.- (0 /,--4 '(+."-"! /( )+7= ,( H(X "( 4#,,4- ,#)-@! I(H28E" 4-7,+.- *.-"-$," )2,-.#24" 0(.

    +"- #$ 2$8 ",--4 7(+."- ,=2, =2" "()-H-%.-- (0 0(7+" ($ +$H-.",2$H#$% ,=-6-=2

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    '=244-$%- (0 >-"#%$#$%

    /,--4 /,.+7,+.-"/,.-$%,=[

    Q-#%=,/,#00$-""[

    Q-#%=,'()*-,#,#

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    '=244-$%- (0 >-"#%$#$%

    /,--4 /,.+7,+.-"! !$H-.",2$H#$% /,.+7,+.24 /,26#4#,8" O-$-.24 T-=2

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    N=8"#724 526"1(+4H 6- #H-24X6+,@ &'() *+),-. /012'.'03 4567)80+

    ab c+.2

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    /()- ?#",(.8@ABCDE"F! N.(H+7, (0 -H+72,#($24 "(0,12.-

    " T/'U dCeX GUfO dCgX N=> dCh`EBA! '(.$-44 'UU M27+4,8 4-H ,=- 128

    " G7O+#.-X L6-4X P$%.200-2X O-.%-48X >-#-.4-#$" >-

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    /()- ?#",(.8@ABCDE"F! G7O+#.-E" /,--4 >-"#%$ '(+."-"

    " !$H-.",2$H 6-=2

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    3#.,+24 526(.2,(.8! M2", 0(.12.H ,( ,=- 42,- BDE"

    " O!P 0(. 2$248"#" "(0,12.- #" ,=- $(.)" M27+4,8 H-

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    3#.,+24 526(.2,(.8! P$ -2.48 mDDD@

    " $109'; /09-70-91.

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    3#.,+24 526(.2,(.8! mDDD`mDAD@

    " U42",#7 $($4#$-2. (*,#($" 6-7()- ,=- $(.) #$7())-.7#24 2$248"#" "(0,12.-

    " ;,=-. -H+72,#($24[.-"-2.7= 2$248"#" "(0,12.- #"H-

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    AmXBeC G2,426 3-."#($ABXmeg N'`

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    3#.,+24 526(.2,(.8!

    f--H" 0(. "#)+42,#$% ",.+7,+.24 ",26#4#,8 *.(64-)"" N2.,#24 8#-4H#$% 277-$,+2,-H 68 .-"#H+24 ",.-""-"" M+44 7.(""`"-7,#($ 8#-4H#$%X *42",#7 =#$%-" 5(724 6+7J4#$%X -42",#7[#$-42",#7"

    M4-^+.24 6+7J4#$%X -42",#7[#$-42",#7" I(."#($24 6+7J4#$%X -42",#7[#$-42",#7" 52,-.24`,(."#($24 6+7J4#$%X -42",#7[#$-42",#7" M4-^+.24`,(."#($24 6+7J4#$%X -42",#7[#$-42",#7" L6(

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    3#.,+24 526(.2,(.8! /#)+42,#$% /,.+7,+.24 /,26#4#,8

    " "-PfLX Lf/c/X NU9M;9Gj>X 5L9/Le>X@

    " UH+72,#($24 MUL "(0,12.-;*-$/--"X MUppmDAmX OI`/LT9UX TL/NX L.72H-X>.b M.2)-X OTI!5X GL/ILfmX @

    ! '($"#H-.2,#($" 0(. )2J#$% ,=- 7=(#7-" N.#7- 2$H 2

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    3#.,+24 526(.2,(.8

    Q=2, #0kAb H#00-.-$, +$6.27-H 4-$%,= : 2Smb H#00-.-$, Q`"=2*- #" -)*4(8-HSjb H#00-.-$, 4(2H#$% 7($H#,#($"Seb H#00-.-$, "+**(., 7($H#,#($"Sgb #$-42",#7 -00-7," -^[#$74+H-HSnb #)*-.0-7,#($ -^[#$74+H-HShb 12.*#$% -^[#$74+H-HS

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    L-"#%$ 68 ,=- >#.-7, L$248"#" G-,=(H

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    5GAb U42",#7 '(4+)$ T+7J4#$%

    2$H ,=- U00-7, (0 U$H 9-",.2#$,5-2.$#$% ;6l-7,#

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    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    )a(

    )b( )c(

    )d( )e(

    )f (

    delkcuBinmuloc

    esa

    f oepahsybnwohss

    en

    er oe

    ac K ea .0

    .0 01

    0.1 02

    02

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

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    Compute 10 modes

    P = 1 k

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    . . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )

    ) )c(

    )d( )e(

    f

    delcuimuoldeha

    f oeasybwoss

    eni

    ter eT

    lac eulav 5.0

    .

    7.0 .1

    . .

    0.1 0.2

    . .

    .2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

    Mode 1:

    Pcr

    = 273.6

    K = ! L

    EI P

    cr

    = 2.0

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    Mode 2:

    Pcr

    = 273.6

    K = ! L

    EI P

    cr

    = 2.0. . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )

    ) )c(

    )d( )e(

    f

    delcuimuoldeha

    f oeasybwoss

    eni

    ter eT

    lac eulav 5.0

    .

    7.0 .1

    . .

    0.1 0.2

    . .

    .2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

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    Mode 3:

    Pcr

    = 1094.5

    K = ! L

    EI P

    cr

    = 1.0. . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )

    ) )c(

    )d( )e(

    f

    delcuimuoldeha

    f oeasybwoss

    eni

    ter eT

    lac eulav 5.0

    .

    7.0 .1

    . .

    0.1 0.2

    . .

    .2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

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    Mode 4:

    Pcr

    = 1094.5

    K = ! L

    EI P

    cr

    = 1.0. . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )

    ) )c(

    )d( )e(

    f

    delcuimuoldeha

    f oeasybwoss

    eni

    ter eT

    lac eulav 5.0

    .

    7.0 .1

    . .

    0.1 0.2

    . .

    .2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

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    . . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )a(

    )b( )(

    d )

    )f (

    delkcuBnmuloc

    ldehsd

    f opahybnwohss

    enil

    iteohT

    la eua 5.

    .

    7. 0.1

    . .

    .1 .2

    . .

    0.2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

    Mode 5:

    Pcr

    = 2239.2

    K = ! L

    EI P

    cr

    = 0.7

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    . . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )

    ) )c(

    )d( )e(

    f

    delcuimuoldeha

    f oeasybwoss

    eni

    ter eT

    lac eulav 5.0

    .

    7.0 .1

    . .

    0.1 0.2

    . .

    .2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

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    . . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )

    ) )c(

    )d( )e(

    f

    delcuimuoldeha

    f oeasybwoss

    eni

    ter eT

    lac eulav 5.0

    .

    7.0 .1

    . .

    0.1 0.2

    . .

    .2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

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    . . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )

    ) )c(

    )d( )e(

    f

    delcuimuoldeha

    f oeasybwoss

    eni

    ter eT

    lac eulav 5.0

    .

    7.0 .1

    . .

    0.1 0.2

    . .

    .2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

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    . . .

    Buckled shape ofcolumn is shown bydashed line

    (a) (b) (c) (d) (e) (f)

    Theoretical K value 0.5 0.7 1.0 1.0 2.0 2.0

    . . . . . .

    )a(

    )b( )

    d )e

    )f (

    delkcBnmuloc

    lesd

    f opahsynwohss

    enl

    iter ohT

    a eua 5.

    .

    7. 0.1

    . .

    .1 .2

    . .

    0.2

    .

    TABLE C-A-7.1Approximate Values of Effective

    Length Factor, K

    Mode 9:

    Pcr

    = 4380

    K = ! L

    EI P

    cr

    = 0.5

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    Dbg

    Dbn

    Dbh

    DbC

    DbB

    A

    D

    gDD

    ADDD

    AgDD

    mDDD

    mgDD

    jDDD

    jgDD

    eDDD

    egDD

    gDDD

    D gDD ADDD AgDD mDDD mgDD

    ! ; +

    & 2 $ , #

    " 2 #

    < 3 " = >

    5,?1@$ ,+ A@1#$"&

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    Vary beam sizes w/

    I Top Beam

    ! I Bottom Beam

    C 027,(.

    ! 7.> I(*> T(,,()

    > I(*

    > T(,,()

    AbD

    Dbg

    I=2$J" ,(c+- ?+2

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    5Gmb M27,(." P$W4+-$7#$% ,=-M4-^+.24 T+7J4#$% /,.-$%,= (0

    '()*.-""#($ G-)6-."5-2.$#$% ;6l-7,#

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    & 8

    U+4-.

    LP/'

    $( " ( [ $( $ .-"" ( [ $( $ .-"

    $( " ( [ $ .-"" ( [ $ .-"

    U'5P'5

    !

    !

    I=2$J" ,( >2$ I2)2.J#$

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    I = 2 $

    J " , (

    T + 4 - $ ,

    L 4 - )

    H 2 . 2 ,

    T - $ , 4 - 8

    F

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    & 8

    U+4-.

    LP/'

    $( " ( [ $( $ .-"" ( [ $( $ .-"

    $( " ( [ $ .-"" ( [ $ .-"

    U'5

    P'5

    I=2$J" ,( >2$ I2)2.J#$

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    5Gjb U00-7,#

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    /#H-128" 4-2$#$%X 1-"#H-128" H2.,-Hq -

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    !"#$%"&'()+,-'#($&'

    "&). /"# 0$1,-2(.3&4$5$',1 6(-,-

    7,/'

    6")89&

    +$:4'

    6")89&

    ;"< =,(9

    ="''"9 =,(9

    >?@A?B

    C

    D @ A ? B

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    !" #$%&' !"#$%&' ()*')+% ,+)" #$%&' ,+)"#$%&' ()*')+%

    -*&%&'#" ."&/+0)+% 1&22)*)+') -*&%&'#" ."&/+0)+% 1&22)*)+')

    34#5 -6#*%$ 789 34#5 -6#*%$ 789

    : ;?@ ;

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    5Geb M27,(." P$W4+-$7#$% ,=-

    /,.-$%,= (0 M4-^+.24 G-)6-."5-2.$#$% ;6l-7,#

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    5Ge! QAe^gj YLBBmZ! : 2 u Abm ,( jAbA 0,b

    ! M(. -27= : 2X #$

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    ! !

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    M n / M p

    ! !

    L p Lr

    I=2$J" ,( >2$ I2)2.J#$

    Lb

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    5Ggb 52,-.24`I(."#($24 T+7J4#$%

    (0 T-2)" 1#,= G()-$, O.2H#-$,5-2.$#$% ;6l-7,#

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    5Gg

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    5Gg!

    !!

    #

    "

    # $

    "!"#

    !%#

    !

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    G A u `ADDD #$`J

    G m u ADDD #$`J

    G 7. u jnDAbC #$`J

    G A u `ADDD #$`J

    G m u `nDD #$`J

    G 7. u BhChbj #$`J

    C b

    MASTAN 2=

    9787.3

    3601.8= 2.72

    C b

    AISC = 2.19

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    I=2$J" ,( c+- ?+2

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    Q($% 2$H >.#

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    I#)- 0(. 8(+ ,( ,2J- #, 0(. 2 "*#$@

    W24x68 with L = 24 ft. (288 in.)M1 = -1000 in-k

    M2 = +1000 in-k

    u jnDm J#*`#$u jDD J#*`0,

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    !!

    !#

    !"#

    W24x68

    Mcr (kip-in) Case 1 Case 2

    M1/M2 = -1

    M1/M2 = +1

    Case 1: Braces at endsCase 2: Braces at ends

    and mid-span

    Observations :

    L =24 ft. (288 in.)

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    !!

    !#

    !"#

    W24x68

    Mcr (kip-in) Case 1 Case 2

    M1/M2 = -1 3,602 12,120

    M1/M2 = +1 9,838 27,414

    Case 1: Braces at endsCase 2: Braces at ends

    and mid-span

    Observations :

    L =24 ft. (288 in.)

    3.36

    Mcr increases as L b is reduced

    2.73

    Mcr increases as moment gradient increases An inflection point is not a brace point!

    2.79

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    5Gnb T-2) >-"#%$ 68 U42",#7

    2$H P$-42",#7 L$248"-"5-2.$#$% ;6l-7,#

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    ]N.-H#7,#($ #" 2$#"= N=8"#7#",

    YACCg ` ABnmZ

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    5Gnk U42",#7 -"#%$!

    "

    "#$%&' ($%&' "#$%&' )$%&'

    * + , -

    B /&414CAb L44 )-)6-." W16x31, P u = SmbW27x84, W16x31, W18x35, P u= Sjb L44 )-)6-." "2)- "#R-X P u = 200k X )#$b 1-#%=,S

    eb G-)6-." "#R-" )28

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    W27x84 W16x31 W18x35

    100 kip

    Case 2: Inelastic Analysis

    P u = 101.3 kip Wt = 1.881 kip P u / Wt = 53.84

    !"

    "#$%&' ($%&' "#$%&' )$%&'

    * + , -

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    !"#$ !% %$ $& ! " '()*+ ,-*./) '()*+&-0*.1 3-)/+4 56789: 5;789: 0 ! " ?! "#$%&'()*$+ =*>0 ! " ? ,*

    (@ AB(0)*C ,5DEF5 ,5DEF5 ,5DEF5 ;G@6F 9@;H5 5@69< I9@G9J@ AB(0)*C

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    5Ghb /-7($H`(.H-. U00-7,"Y! `s 2$H ! `tZ U00-7,"

    5-2.$#$% ;6l-7,#

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    %&''( )'*+,- . /0' /1(' 23 /425+&+'*

    P, 12" ,=- 6-", (0 ,#)-"Y*4+%E$ 7=+% ,=- -V+2,#($" 2$H

    6-#$% 264- 1#,= ,=- ,264-Z#, 12" ,=- 1(.", (0 ,#)-"

    Y6-#$% .-"*($"#64- 0(. .-2448+$H-.",2$H#$% ,=- 6-=2

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    A", (.H-.

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    M max1st

    = 200 k-in

    M max2nd= 391 k-in

    B1Computation

    =

    391200

    = 1.96

    M 1

    1st= ! 150 k-in

    M 21st = + 200 k-in = M max1st( )C

    m = 0.6 ! 0.4 ! 150 + 200( )= 0.9

    P Pe

    = 0.5 B1

    AISC=

    0.9

    1 ! 0.5= 1.8

    M max

    2nd= B

    1

    AISC M max

    1st

    M max

    2nd= 1.8 " 200 =360 k-in

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    !

    #

    $

    %

    &

    '!

    '#

    ! !(' !(# !() !($ !(* !(% !(+ !(& !(, '

    ! " # $ % &

    ( ) )

    * + , - . + & " %

    / 0 1

    232$

    #-./01.21 234567 89:;

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    5GCb /,.-$%,= (0 T-2)`'(4+)$"5-2.$#$% ;6l-7,#

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